View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 61629U 26144.84506838 +.00000000 +00000-0 +93914-5 0 00007
2 61629 43.0017 84.3953 0001391 281.4628 78.6068 15.27574955 03
| Epoch (UTC): | 24 May 2026 20:16:53 |
| Eccentricity: | 0.0001391 |
| inclination: | 43.0017° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 84.3953° |
| argument of perigee: | 281.4628° |
| revolutions per day: | 15.27574955 |
| mean anomaly at epoch: | 78.6068° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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