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 57999U 26145.27009637 +.00000000 +00000-0 +13764-3 0 00008
2 57999 42.9992 354.9740 0001463 283.6628 76.4061 15.27582354 03
| Epoch (UTC): | 25 May 2026 06:28:56 |
| Eccentricity: | 0.0001463 |
| inclination: | 42.9992° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 354.9740° |
| argument of perigee: | 283.6628° |
| revolutions per day: | 15.27582354 |
| mean anomaly at epoch: | 76.4061° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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