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N1-ATLAS

In orbit NORAD 68501 EIQV-9761-1647-1492-5660

Falcon 9 Block 5

Carrier rocket

Space Launch Complex 4E

Spaceport

0

Observations all time

Mission information
Spacecraft name
N1-ATLAS
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
Separation time
Satellite appearance
Data for the last 30 days
Orbital parameters of the satellite
Perigee
586.69 km
Apogee
591.90 km
Inclination
97.8°
Period
96.5 min
Semi-major axis
6967.4 km
Velocity
7.56 km/s
Orbital elements
TLE source
Celestrak
TLE updated
2026-10-14 14:09:05 UTC
Two-line elements (TLE)
1 68501U 26067CP  26287.13933477  .00001581  00000-0  16229-3 0  9991
2 68501 97.7787 243.6485 0003735 19.5859 340.5503 14.91815903 29455
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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
2026-10-15 09:12:03 VINDLER 2.3
NORAD 68486
N1-ATLAS
NORAD 68501
4.451 0.00 7.5e-08
2026-10-15 10:08:02 N1-ATLAS
NORAD 68501
ORBCOMM FM111
NORAD 40089
3.505 10.38 2.7e-07
2026-10-15 10:14:55 VINDLER 2.3
NORAD 68486
N1-ATLAS
NORAD 68501
4.937 0.01 1.8e-07
2026-10-15 12:44:58 VINDLER 2.2
NORAD 68484
N1-ATLAS
NORAD 68501
3.180 0.12 4.4e-07
2026-10-15 13:33:13 VINDLER 2.2
NORAD 68484
N1-ATLAS
NORAD 68501
2.458 0.12 7.3e-07
2026-10-15 16:46:23 LEMUR-2-SEJONG-3
NORAD 68482
N1-ATLAS
NORAD 68501
4.687 0.04 2.0e-07
2026-10-16 03:53:18 HUBBLE 7
NORAD 64592
N1-ATLAS
NORAD 68501
2.782 14.69 2.3e-07
2026-10-16 04:22:18 VINDLER 2.1
NORAD 68488
N1-ATLAS
NORAD 68501
3.098 0.00 2.3e-07
2026-10-16 08:52:01 LEMUR-2-IRINA
NORAD 68480
N1-ATLAS
NORAD 68501
3.796 0.06 3.1e-07
2026-10-17 13:48:18 N1-ATLAS
NORAD 68501
IRIDIUM 33 DEB
NORAD 35797
3.215 7.67 3.8e-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