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 57654U 26145.62676115 +.00000000 +00000-0 +11578-3 0 00007
2 57654 97.9131 63.9684 0001677 92.5059 267.6345 14.80176786 07
| Epoch (UTC): | 25 May 2026 15:02:32 |
| Eccentricity: | 0.0001677 |
| inclination: | 97.9131° |
| perigee height: | 628 km |
| apogee height: | 630 km |
| right ascension of ascending node: | 63.9684° |
| argument of perigee: | 92.5059° |
| revolutions per day: | 14.80176786 |
| mean anomaly at epoch: | 267.6345° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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