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 61051U 26145.43810473 +.00000000 +00000-0 +38427-4 0 00002
2 61051 53.1554 292.8850 0000986 74.1057 286.0069 15.69722068 06
| Epoch (UTC): | 25 May 2026 10:30:52 |
| Eccentricity: | 0.0000986 |
| inclination: | 53.1554° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 292.8850° |
| argument of perigee: | 74.1057° |
| revolutions per day: | 15.69722068 |
| mean anomaly at epoch: | 286.0069° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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