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 49403U 21102J 24358.12073456 .00028650 00000-0 10896-2 0 9993
2 49403 97.3961 45.6107 0012634 292.3707 67.6193 15.26659330172031
| Epoch (UTC): | 23 December 2024 02:53:51 |
| Eccentricity: | 0.0012634 |
| inclination: | 97.3961° |
| perigee height: | 477 km |
| apogee height: | 494 km |
| right ascension of ascending node: | 45.6107° |
| argument of perigee: | 292.3707° |
| revolutions per day: | 15.26659330 |
| mean anomaly at epoch: | 67.6193° |
| orbit number at epoch: | 17203 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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