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 57710U 26145.12261778 +.00000000 +00000-0 +52781-4 0 00002
2 57710 43.0046 46.1115 0001215 256.1905 103.8811 15.27586965 00
| Epoch (UTC): | 25 May 2026 02:56:34 |
| Eccentricity: | 0.0001215 |
| inclination: | 43.0046° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 46.1115° |
| argument of perigee: | 256.1905° |
| revolutions per day: | 15.27586965 |
| mean anomaly at epoch: | 103.8811° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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