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 57912U 26145.55120950 +.00000000 +00000-0 +50086-3 0 00004
2 57912 43.0011 236.5116 0001280 268.8480 91.2225 15.27592675 06
| Epoch (UTC): | 25 May 2026 13:13:44 |
| Eccentricity: | 0.0001280 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 236.5116° |
| argument of perigee: | 268.8480° |
| revolutions per day: | 15.27592675 |
| mean anomaly at epoch: | 91.2225° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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