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 57795U 26145.55436259 +.00000000 +00000-0 +66770-4 0 00003
2 57795 49.9729 248.0123 0014236 182.4128 177.6717 14.23131590 02
| Epoch (UTC): | 25 May 2026 13:18:16 |
| Eccentricity: | 0.0014236 |
| inclination: | 49.9729° |
| perigee height: | 805 km |
| apogee height: | 825 km |
| right ascension of ascending node: | 248.0123° |
| argument of perigee: | 182.4128° |
| revolutions per day: | 14.23131590 |
| mean anomaly at epoch: | 177.6717° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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