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 57975U 26145.33138329 +.00000000 +00000-0 +36308-3 0 00009
2 57975 42.9956 263.4935 0000536 51.7726 308.3174 15.27602089 00
| Epoch (UTC): | 25 May 2026 07:57:11 |
| Eccentricity: | 0.0000536 |
| inclination: | 42.9956° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 263.4935° |
| argument of perigee: | 51.7726° |
| revolutions per day: | 15.27602089 |
| mean anomaly at epoch: | 308.3174° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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