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 26857U 26145.55134029 +.00000000 +00000-0 +00000-0 0 00008
2 26857 44.8381 250.4814 0014976 49.6928 310.4678 3.92401455 09
| Epoch (UTC): | 25 May 2026 13:13:55 |
| Eccentricity: | 0.0014976 |
| inclination: | 44.8381° |
| perigee height: | 10576 km |
| apogee height: | 10626 km |
| right ascension of ascending node: | 250.4814° |
| argument of perigee: | 49.6928° |
| revolutions per day: | 3.92401455 |
| mean anomaly at epoch: | 310.4678° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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