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NORBI

In orbit NORAD 46494 DNNN-7162-2135-4056-8903 Russia

Time in UTC

07:20

Next pass · Чукотка · 15°

—

No observations scheduled

117

Observations over 30 days

36%

Successful observations

2k

Frames, latest 2026-10-10 14:24 UTC

Mission information
Spacecraft name
NORBI
Other names
NORBY
Call sign
-
Network
УниверСат
Status
Active
The satellite is in orbit
Launch and timeline
Launch time
Separation time
Last observers
Observer
Time of receipt
2026-10-10 14:24:24 UTC
2026-10-09 16:45:38 UTC
2026-10-09 15:16:11 UTC
2026-10-08 14:32:14 UTC
2026-10-08 05:32:48 UTC
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
400.08 km
Apogee
407.97 km
Inclination
97.9°
Period
92.7 min
Semi-major axis
6782.1 km
Velocity
7.67 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-13 06:09:02 UTC
Two-line elements (TLE)
1 46494U 20068J   26285.90970130  .00028672  00000-0  45482-3 0  9996
2 46494 97.8551 312.6640 0005862 164.7166 195.4264 15.53330035334456
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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
2026-10-13 13:39:25 NORBI
NORAD 46494
CZ-6A DEB
NORAD 61327
4.000 7.94 2.4e-07
2026-10-14 20:29:12 NORBI
NORAD 46494
USA 77
NORAD 21809
4.655 13.38 1.2e-07
2026-10-16 02:43:52 NORBI
NORAD 46494
BRO-5
NORAD 51061
4.914 6.17 1.7e-07
2026-10-19 01:41:47 NORBI
NORAD 46494
STARLINK-38416
NORAD 100638
3.209 15.02 4.9e-06
2026-10-19 02:28:11 NORBI
NORAD 46494
STARLINK-38416
NORAD 100638
3.994 15.05 3.2e-06

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