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 57512U 26145.37051054 +.00000000 +00000-0 +38556-4 0 00007
2 57512 43.0031 277.2267 0002271 284.5205 75.5394 15.27576031 04
| Epoch (UTC): | 25 May 2026 08:53:32 |
| Eccentricity: | 0.0002271 |
| inclination: | 43.0031° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 277.2267° |
| argument of perigee: | 284.5205° |
| revolutions per day: | 15.27576031 |
| mean anomaly at epoch: | 75.5394° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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