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 61896U 26145.65439705 +.00000000 +00000-0 +48751-3 0 00008
2 61896 97.4131 217.1424 0053174 81.0856 279.6389 15.11984379 08
| Epoch (UTC): | 25 May 2026 15:42:19 |
| Eccentricity: | 0.0053174 |
| inclination: | 97.4131° |
| perigee height: | 493 km |
| apogee height: | 567 km |
| right ascension of ascending node: | 217.1424° |
| argument of perigee: | 81.0856° |
| revolutions per day: | 15.11984379 |
| mean anomaly at epoch: | 279.6389° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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