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 57651U 26145.34382525 +.00000000 +00000-0 -11434-5 0 00006
2 57651 42.9961 8.2950 0001232 67.2882 292.8100 15.27560806 04
| Epoch (UTC): | 25 May 2026 08:15:06 |
| Eccentricity: | 0.0001232 |
| inclination: | 42.9961° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 8.2950° |
| argument of perigee: | 67.2882° |
| revolutions per day: | 15.27560806 |
| mean anomaly at epoch: | 292.8100° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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