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STARLINK-3005

In orbit NORAD 48881 IVNB-2417-4826-3529-8699

Observations 0
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Falcon 9 Block 5 | Transporter 2 (Dedicated SSO Rideshare)

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 40

Spaceport

0

Observations all time

Mission information
Spacecraft name
STARLINK-3005
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 | Transporter 2 (Dedicated SSO Rideshare)
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 40
Launch time
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
558.22 km
Apogee
561.70 km
Inclination
97.3°
Period
95.9 min
Semi-major axis
6938.1 km
Velocity
7.56 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-10 04:46:18 UTC
Two-line elements (TLE)
1 48881U 21059C   26282.90290213 -.00000339  00000-0 -22170-4 0  9995
2 48881  97.2865  42.0354 0002506 196.1965 163.9180 15.01270375290949
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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 22:05:35 KAZSTSAT
NORAD 43783 		STARLINK-3005
NORAD 48881 		2.110 10.85 2.2e-05
2026-10-12 20:07:44 RISAT-2BR2
NORAD 46905 		STARLINK-3005
NORAD 48881 		3.367 13.79 6.0e-06
2026-10-16 06:46:41 GRUS-1E
NORAD 47935 		STARLINK-3005
NORAD 48881 		1.989 13.10 1.9e-05

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