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 61231U 26145.37157362 +.00000000 +00000-0 +66058-4 0 00007
2 61231 97.4121 217.9705 0001605 87.9850 272.1569 15.19184299 00
| Epoch (UTC): | 25 May 2026 08:55:03 |
| Eccentricity: | 0.0001605 |
| inclination: | 97.4121° |
| perigee height: | 507 km |
| apogee height: | 509 km |
| right ascension of ascending node: | 217.9705° |
| argument of perigee: | 87.9850° |
| revolutions per day: | 15.19184299 |
| mean anomaly at epoch: | 272.1569° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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