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 25861U 26138.11789367 +.00000000 +00000-0 +43295-4 0 00004
2 25861 97.9856 197.0641 0015560 36.8726 323.3554 14.81811921 06
| Epoch (UTC): | 18 May 2026 02:49:46 |
| Eccentricity: | 0.0015560 |
| inclination: | 97.9856° |
| perigee height: | 613 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 197.0641° |
| argument of perigee: | 36.8726° |
| revolutions per day: | 14.81811921 |
| mean anomaly at epoch: | 323.3554° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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