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 48247U 21032A 25228.99004365 0.00000700 00000-0 93682-4 0 00
2 48247 98.0830 342.8275 0154125 107.3157 252.6841 14.71511175 09
| Epoch (UTC): | 16 August 2025 23:45:39 |
| Eccentricity: | 0.0154125 |
| inclination: | 98.0830° |
| perigee height: | 548 km |
| apogee height: | 764 km |
| right ascension of ascending node: | 342.8275° |
| argument of perigee: | 107.3157° |
| revolutions per day: | 14.71511175 |
| mean anomaly at epoch: | 252.6841° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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