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NEXTSAT-1

In orbit NORAD 43811 AQBM-4818-7548-5694-3468

Observations 0
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Falcon 9 Block 5 | Spaceflight SSO-A

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
NEXTSAT-1
Status
Active
The satellite is in orbit
The network has not received data from this satellite for a long time
Launch and timeline
Launch
Falcon 9 Block 5 | Spaceflight SSO-A
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
528.62 km
Apogee
543.35 km
Inclination
97.4°
Period
95.4 min
Semi-major axis
6914.1 km
Velocity
7.59 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 12:56:47 UTC
Two-line elements (TLE)
1 43811U 18099BF  26283.05318574  .00002149  00000-0  13938-3 0  9991
2 43811  97.3955 321.7082 0010651 306.2623  53.7622 15.09081067429204
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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
2026-10-11 01:31:55 NEXTSAT-1
NORAD 43811 		OBJECT E
NORAD 66997 		4.965 4.66 1.7e-07
2026-10-12 04:52:45 NEXTSAT-1
NORAD 43811 		STARLINK-5479
NORAD 55662 		3.553 4.01 1.0e-05
2026-10-12 10:12:20 NEXTSAT-1
NORAD 43811 		FENGYUN 1C DEB
NORAD 29865 		3.473 10.33 2.8e-07
2026-10-12 10:58:30 NEXTSAT-1
NORAD 43811 		OBJECT B
NORAD 61239 		3.230 4.93 4.0e-07
2026-10-12 14:02:31 NEXTSAT-1
NORAD 43811 		COSMOS 2251 DEB
NORAD 34452 		2.994 7.51 4.4e-07
2026-10-12 18:55:49 NEXTSAT-1
NORAD 43811 		PSLV DEB
NORAD 35344 		4.313 2.37 2.3e-07
2026-10-13 11:32:50 NEXTSAT-1
NORAD 43811 		STARLINK-5289
NORAD 55278 		4.793 12.56 3.6e-06
2026-10-13 11:54:02 NEXTSAT-1
NORAD 43811 		A-1 (ASTERIX)
NORAD 1778 		3.197 9.78 3.5e-07
2026-10-15 20:54:27 NEXTSAT-1
NORAD 43811 		OBJECT C
NORAD 68200 		2.978 4.45 4.8e-07
2026-10-16 03:43:27 NEXTSAT-1
NORAD 43811 		STARLINK-4513
NORAD 53548 		2.233 14.67 1.1e-05
2026-10-16 16:49:42 NEXTSAT-1
NORAD 43811 		IMS-1
NORAD 32786 		3.581 6.17 3.2e-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