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 48892U 21059P 24358.15312615 .00004327 00000-0 59957-3 0 9998
2 48892 95.9796 199.8214 0011672 65.4283 294.8148 14.78261590188205
| Epoch (UTC): | 23 December 2024 03:40:30 |
| Eccentricity: | 0.0011672 |
| inclination: | 95.9796° |
| perigee height: | 626 km |
| apogee height: | 643 km |
| right ascension of ascending node: | 199.8214° |
| argument of perigee: | 65.4283° |
| revolutions per day: | 14.78261590 |
| mean anomaly at epoch: | 294.8148° |
| orbit number at epoch: | 18820 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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