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UNICORN-2R

In orbit NORAD 68477 IQBQ-2020-5200-0150-7482

Observations 83
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2026

Falcon 9 Block 5 | Transporter 16 (Dedicated SSO Rideshare)

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

83

Observations all time

Mission information
Spacecraft name
UNICORN-2R
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 16 (Dedicated SSO Rideshare)
Carrier rocket
Falcon 9 Block 5
Spaceport
Space Launch Complex 4E
Launch time
2026-03-30 11:02:00
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
580.27 km
Apogee
588.66 km
Inclination
97.8°
Period
96.4 min
Semi-major axis
6962.6 km
Velocity
7.57 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-11 04:56:40 UTC
Two-line elements (TLE)
1 68477U 26067BP  26283.64201963  .00009974  00000-0  95493-3 0  9997
2 68477  97.7636 240.0814 0006023  58.7794 301.4016 14.93365302 28351
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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 22:52:20 UNICORN-2R
NORAD 68477 		COSMOS 397
NORAD 4964 		3.449 4.70 3.5e-07
2026-10-11 23:06:35 UNICORN-2R
NORAD 68477 		SCOUT X-4 R/B
NORAD 1815 		4.976 11.79 1.6e-07
2026-10-12 00:37:38 IRIDE-MS2-HEO-8
NORAD 64587 		UNICORN-2R
NORAD 68477 		0.467 14.65 8.2e-06
2026-10-13 18:36:05 UNICORN-2R
NORAD 68477 		IO-1
NORAD 68498 		2.968 0.01 5.0e-07
2026-10-15 01:04:47 FIREFLY-2
NORAD 62704 		UNICORN-2R
NORAD 68477 		3.435 12.88 2.2e-07
2026-10-15 01:53:01 FIREFLY-2
NORAD 62704 		UNICORN-2R
NORAD 68477 		3.920 12.92 1.7e-07
2026-10-15 17:10:31 UNICORN-2R
NORAD 68477 		PSLV DEB
NORAD 27141 		1.495 11.40 1.4e-06
2026-10-15 18:48:20 UNICORN-2R
NORAD 68477 		METEOR 2-6 DEB
NORAD 28987 		4.132 14.77 1.0e-07
2026-10-15 18:48:35 UNICORN-2R
NORAD 68477 		ICEYE-X75
NORAD 68497 		3.613 0.03 3.4e-07
2026-10-15 20:24:51 UNICORN-2R
NORAD 68477 		METEOR 2-6 DEB
NORAD 28987 		4.519 14.77 8.3e-08
2026-10-16 08:47:59 UNICORN-2R
NORAD 68477 		CZ-6A DEB
NORAD 60854 		2.501 1.25 7.0e-07
2026-10-17 04:34:51 UNICORN-2R
NORAD 68477 		FENGYUN 1C DEB
NORAD 29866 		3.085 3.65 4.5e-07
2026-10-17 06:34:12 UNICORN-2R
NORAD 68477 		CZ-2C DEB
NORAD 28483 		4.067 15.00 9.6e-08

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