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 61929U 26145.45612134 +.00000000 +00000-0 +68488-3 0 00001
2 61929 42.9990 208.1031 0001720 279.7432 80.3225 15.27598919 07
| Epoch (UTC): | 25 May 2026 10:56:48 |
| Eccentricity: | 0.0001720 |
| inclination: | 42.9990° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 208.1031° |
| argument of perigee: | 279.7432° |
| revolutions per day: | 15.27598919 |
| mean anomaly at epoch: | 80.3225° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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