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 61637U 26145.51306897 +.00000000 +00000-0 -15777-4 0 00005
2 61637 43.0014 80.8078 0000562 256.1078 103.9711 15.27570771 04
| Epoch (UTC): | 25 May 2026 12:18:49 |
| Eccentricity: | 0.0000562 |
| inclination: | 43.0014° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 80.8078° |
| argument of perigee: | 256.1078° |
| revolutions per day: | 15.27570771 |
| mean anomaly at epoch: | 103.9711° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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