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CARTOSAT-2A

In orbit NORAD 32783 DHND-4474-1527-7198-0174 ISRO India

2008

Launch

0

Observations all time

military satellite

Mission description
Mission information
Spacecraft name
CARTOSAT-2A
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch time
2008-04-28 00:00:00
Separation time
Satellite appearance
Operator
ISRO
Data for the last 30 days
Orbital parameters of the satellite
Perigee
619.05 km
Apogee
637.72 km
Inclination
97.7°
Period
97.3 min
Semi-major axis
7006.5 km
Velocity
7.54 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-16 06:36:24 UTC
Two-line elements (TLE)
1 32783U 08021A   26288.98817388  .00000074  00000-0  16605-4 0  9995
2 32783 97.7492 333.4922 0013326 79.6438 280.6276 14.79355721996662
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Orbit history, past year

Mean elements of every TLE set over the past 365 days, plotted against the epoch of the set. Each source is its own line; click it in the legend to hide it. A jump in altitude is a manoeuvre or a bad set; lines drifting apart are a disagreement between sources. “TLE age” is how many hours have passed since the epoch of the source's freshest set, plotted against when the set reached us, on a logarithmic scale. A set the source repeats unchanged does not reset the age.

Prediction divergence

Each TLE set is propagated with SGP4 to the epoch of the next set from the same source and compared with it, plotted against the epoch of the next set; the tooltip shows how many hours ahead the prediction ran. The logarithmic scale shows the size of the divergence and the tooltip its sign: plus along-track means the prediction is ahead of the satellite. This is how well the sets agree, not the true error: the reference is a TLE too, off by about a kilometre. An outlier is a manoeuvre between sets. Sets more than a week apart are not compared.

Time of closest approach, UTC Object 1 Object 2 Distance, km Speed, km/s Max. probability
2026-10-17 01:14:40 CARTOSAT-2A
NORAD 32783
FENGYUN 1C DEB
NORAD 29933
4.897 10.22 1.4e-07
2026-10-17 15:52:55 CARTOSAT-2A
NORAD 32783
COSMOS 1275 DEB
NORAD 12773
0.385 13.96 1.4e-05
2026-10-17 19:38:48 CARTOSAT-2A
NORAD 32783
KUIPER-00191
NORAD 67143
4.638 14.46 8.8e-08
2026-10-17 21:48:08 CARTOSAT-2A
NORAD 32783
KUIPER-00072
NORAD 64819
4.047 7.78 2.4e-07
2026-10-18 10:44:40 CARTOSAT-2A
NORAD 32783
KUIPER-00598
NORAD 69768
0.864 13.31 3.3e-06
2026-10-19 00:16:49 CARTOSAT-2A
NORAD 32783
ARIRANG-1 (KOMPSAT-1)
NORAD 26032
4.393 13.55 1.2e-07
2026-10-19 00:58:11 CARTOSAT-2A
NORAD 32783
KUIPER-00608
NORAD 69291
4.235 13.70 1.3e-07
2026-10-19 02:35:32 CARTOSAT-2A
NORAD 32783
KUIPER-00608
NORAD 69291
4.427 13.71 1.2e-07
2026-10-19 03:01:31 CARTOSAT-2A
NORAD 32783
KUIPER-00169
NORAD 65782
1.576 14.11 8.4e-07
2026-10-19 04:38:51 CARTOSAT-2A
NORAD 32783
KUIPER-00169
NORAD 65782
4.986 14.10 8.4e-08
2026-10-19 05:05:05 CARTOSAT-2A
NORAD 32783
FENGYUN 1C DEB
NORAD 32114
3.196 14.40 1.9e-07
2026-10-19 10:58:45 CARTOSAT-2A
NORAD 32783
NOAA 16 DEB
NORAD 41207
3.459 13.20 2.1e-07
2026-10-19 21:45:02 CARTOSAT-2A
NORAD 32783
IRIDIUM 179
NORAD 56730
3.771 1.61 3.1e-07
2026-10-20 11:29:47 CARTOSAT-2A
NORAD 32783
SL-16 DEB
NORAD 27760
4.498 14.99 7.7e-08
2026-10-20 23:39:05 CARTOSAT-2A
NORAD 32783
DELTA 2 R/B
NORAD 25876
2.256 14.00 4.3e-07
2026-10-21 03:15:46 CARTOSAT-2A
NORAD 32783
KUIPER-00608
NORAD 69291
4.269 14.09 1.2e-07
2026-10-21 04:53:06 CARTOSAT-2A
NORAD 32783
KUIPER-00608
NORAD 69291
4.385 14.10 1.1e-07
2026-10-21 08:07:11 CARTOSAT-2A
NORAD 32783
IRIDIUM 33 DEB
NORAD 36390
3.302 15.10 1.4e-07
2026-10-21 10:17:27 CARTOSAT-2A
NORAD 32783
COSMOS 2251 DEB
NORAD 34574
2.688 15.05 2.1e-07
2026-10-21 15:03:09 CARTOSAT-2A
NORAD 32783
KUIPER-00169
NORAD 65782
2.396 13.65 4.0e-07
2026-10-21 16:40:29 CARTOSAT-2A
NORAD 32783
KUIPER-00169
NORAD 65782
3.974 13.63 1.5e-07
2026-10-21 19:33:23 CARTOSAT-2A
NORAD 32783
KUIPER-00108
NORAD 65146
4.761 11.68 1.3e-07

Data: CelesTrak SOCRATES Plus, computed from TLEs of the public catalog. This is an estimate, not grounds for a manoeuvre: TLEs carry no covariance, and the maximum probability assumes a position error.

All conjunctions of this satellite