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 57933U 26145.00315688 +.00000000 +00000-0 +14327-4 0 00000
2 57933 43.0007 253.8474 0000975 278.2741 81.8000 15.27578487 09
| Epoch (UTC): | 25 May 2026 00:04:32 |
| Eccentricity: | 0.0000975 |
| inclination: | 43.0007° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 253.8474° |
| argument of perigee: | 278.2741° |
| revolutions per day: | 15.27578487 |
| mean anomaly at epoch: | 81.8000° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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