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 57774U 26145.41135427 +.00000000 +00000-0 -79516-5 0 00002
2 57774 43.0048 124.3353 0001656 277.2096 82.8568 15.27585964 02
| Epoch (UTC): | 25 May 2026 09:52:21 |
| Eccentricity: | 0.0001656 |
| inclination: | 43.0048° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 124.3353° |
| argument of perigee: | 277.2096° |
| revolutions per day: | 15.27585964 |
| mean anomaly at epoch: | 82.8568° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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