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 57868U 26145.49411111 +.00000000 +00000-0 +24207-4 0 00006
2 57868 43.0016 211.4132 0001284 274.2077 85.8628 15.27577464 03
| Epoch (UTC): | 25 May 2026 11:51:31 |
| Eccentricity: | 0.0001284 |
| inclination: | 43.0016° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 211.4132° |
| argument of perigee: | 274.2077° |
| revolutions per day: | 15.27577464 |
| mean anomaly at epoch: | 85.8628° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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