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 57898U 26145.57129414 +.00000000 +00000-0 -91152-4 0 00004
2 57898 43.0073 240.0745 0001443 270.3703 89.6984 15.27540218 01
| Epoch (UTC): | 25 May 2026 13:42:39 |
| Eccentricity: | 0.0001443 |
| inclination: | 43.0073° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 240.0745° |
| argument of perigee: | 270.3703° |
| revolutions per day: | 15.27540218 |
| mean anomaly at epoch: | 89.6984° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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