Update:The H-IIA rocket body re-entered the Earths atmosphere on the 3rd June, 2012 @ 01:00 GMT ± 45 minutes.
Inclination: 96.97°Revolution Number: 51512Predicted Location: 41.6°S, 259.3°E
Update:The H-IIA rocket body is predicted to re-enter the Earths atmosphere on the 3rd June, 2012 @ 02:00 GMT ± 8 hours.
H-2A RB 1 27700U 03009C 12154.50111901 .05709556 23108-5 54469-3 0 9963 2 27700 096.9685 159.3151 0008827 221.2815 139.0896 16.38508207515043
Period: 88.54 minutesInclination: 96.97°Apogee: 209 kmPerigee: 296 km Revolution Number: 51514Predicted Location: 28°S, 54.3°E
Update:The H-IIA rocket body is predicted to re-enter the Earths atmosphere on the 3rd June, 2012 @ 00:30 GMT ± 24 hours.
H-2A RB 1 27700U 03009C 12153.09074780 .02348595 22261-5 70601-3 0 9907 2 27700 096.9752 157.7765 0008823 180.8280 179.4432 16.26940719514816
Period: 88.91 minutesInclination: 96.98°Apogee: 229 kmPerigee: 213 km Revolution Number: 51512Predicted Location: 0.5°S, 81.6°E
H-2A RB 1 27700U 03009C 12152.53674216 .01644347 22025-5 63254-3 0 9823 2 27700 096.9785 157.1747 0009406 151.7225 208.4460 16.24012422514723
Update:The H-IIA rocket body is predicted to re-enter the Earths atmosphere on the 3rd June, 2012 @ 02:50 GMT ± 48 hours.
H-2A RB 1 27700U 03009C 12152.10529843 .01615445 21979-5 70090-3 0 9810 2 27700 096.9764 156.7127 0008768 171.5231 189.0199 16.22546517514654
Period: 88.91 minutesInclination: 96.98°Apogee: 229 kmPerigee: 213 km Revolution Number: 51515Predicted Location: 46.3°N, 218.4°E
A H-IIA rocket body that was launched on the 28th March, 2003, from the Tanegashima Space Centre, for the IGS 1A and IGS 1B satellite missions is predicted to re-enter the Earths atmosphere on the 8th June, 2012 @ --:-- GMT ± -- hours.
H-2A RB 1 27700U 03009C 12149.19884267 .01032379 70982-3 80735-3 0 9686 2 27700 096.9792 153.6008 0011181 152.8383 207.3283 16.14800884514189
Period: 89.35 minutesInclination: 96.98°Apogee: 250 kmPerigee: 235 km Revolution Number: -Predicted Location: -