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 57701U 26145.12647969 +.00000000 +00000-0 +20026-4 0 00009
2 57701 43.0026 46.1457 0001024 239.0501 121.0250 15.27577349 02
| Epoch (UTC): | 25 May 2026 03:02:07 |
| Eccentricity: | 0.0001024 |
| inclination: | 43.0026° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 46.1457° |
| argument of perigee: | 239.0501° |
| revolutions per day: | 15.27577349 |
| mean anomaly at epoch: | 121.0250° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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