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 57779U 26145.61704516 +.00000000 +00000-0 +50798-4 0 00009
2 57779 43.0027 108.7776 0000960 264.0695 96.0048 15.27573912 05
| Epoch (UTC): | 25 May 2026 14:48:32 |
| Eccentricity: | 0.0000960 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 108.7776° |
| argument of perigee: | 264.0695° |
| revolutions per day: | 15.27573912 |
| mean anomaly at epoch: | 96.0048° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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