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 data is extracted from the following two-line orbital elements,
1 10096U 77055B 25194.34858631 .00000407 00000-0 42033-4 0 9996
2 10096 75.8326 157.6835 0042090 250.3447 109.3201 14.91554435601086
| Epoch (UTC): | 13 July 2025 08:21:57 |
| Eccentricity: | 0.0042090 |
| inclination: | 75.8326° |
| perigee height: | 564 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 157.6835° |
| argument of perigee: | 250.3447° |
| revolutions per day: | 14.91554435 |
| mean anomaly at epoch: | 109.3201° |
| orbit number at epoch: | 60108 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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