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ExseedSat 1

In orbit NORAD 43775 FNPJ-5961-0820-4470-5491 India

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

1

Observations all time

Mission information
Spacecraft name
ExseedSat 1
Other names
VO-96
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2018-12-03 00:00:00
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
528.21 km
Apogee
533.94 km
Inclination
97.4°
Period
95.3 min
Semi-major axis
6909.2 km
Velocity
7.59 km/s
Orbital elements
TLE source
Space-Track.org
TLE updated
2026-10-08 08:46:42 UTC
Two-line elements (TLE)
1 43775U 18099T   26280.64205832  .00001998  00000-0  12443-3 0  9995
2 43775 97.4088 321.3813 0004148 309.6969 50.3895 15.10690304429299
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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
2026-10-12 05:28:59 OBJECT D
NORAD 68201
OBJECT T
NORAD 43775
2.525 4.22 6.7e-07
2026-10-12 09:06:23 OPTICUBE 04
NORAD 41851
OBJECT T
NORAD 43775
2.181 15.04 3.3e-07
2026-10-12 10:41:47 OPTICUBE 04
NORAD 41851
OBJECT T
NORAD 43775
1.739 15.04 5.2e-07
2026-10-12 12:17:11 OPTICUBE 04
NORAD 41851
OBJECT T
NORAD 43775
4.625 15.04 7.4e-08
2026-10-12 14:40:13 OPTICUBE 04
NORAD 41851
OBJECT T
NORAD 43775
4.643 15.05 7.3e-08
2026-10-12 16:15:37 OPTICUBE 04
NORAD 41851
OBJECT T
NORAD 43775
2.940 15.05 1.8e-07
2026-10-12 17:17:58 STARLINK-5288
NORAD 55307
OBJECT T
NORAD 43775
2.133 14.59 1.2e-05
2026-10-12 17:51:01 OPTICUBE 04
NORAD 41851
OBJECT T
NORAD 43775
3.983 15.05 9.9e-08
2026-10-12 18:05:40 STARLINK-5288
NORAD 55307
OBJECT T
NORAD 43775
4.815 14.61 2.4e-06
2026-10-13 07:43:04 OBJECT R
NORAD 57181
OBJECT T
NORAD 43775
3.548 1.54 3.5e-07
2026-10-14 21:04:04 JILIN GAOFEN OBJECT C
NORAD 68693
OBJECT T
NORAD 43775
3.731 4.49 3.0e-07
2026-10-14 22:02:32 STARLINK-6357
NORAD 56783
OBJECT T
NORAD 43775
3.030 14.91 5.5e-06
2026-10-15 03:36:57 STARLINK-4776
NORAD 53837
OBJECT T
NORAD 43775
1.303 9.58 6.3e-05
2026-10-15 06:36:05 UMBRA-09
NORAD 60541
OBJECT T
NORAD 43775
3.008 6.18 4.5e-07
2026-10-15 07:23:46 UMBRA-09
NORAD 60541
OBJECT T
NORAD 43775
3.365 6.17 3.6e-07
2026-10-15 08:11:28 UMBRA-09
NORAD 60541
OBJECT T
NORAD 43775
3.495 6.18 3.3e-07
2026-10-15 19:19:22 JILIN GAOFEN OBJECT A
NORAD 68691
OBJECT T
NORAD 43775
3.598 4.50 3.3e-07
2026-10-16 23:50:04 OBJECT A
NORAD 51946
OBJECT T
NORAD 43775
4.572 12.75 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