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 63492U 25052BN 25321.24797996 .00079242 00000-0 22577-2 0 9993
2 63492 97.4102 214.5427 0009495 145.2645 214.9221 15.35744764 37780
| Epoch (UTC): | 17 November 2025 05:57:05 |
| Eccentricity: | 0.0009495 |
| inclination: | 97.4102° |
| perigee height: | 452 km |
| apogee height: | 465 km |
| right ascension of ascending node: | 214.5427° |
| argument of perigee: | 145.2645° |
| revolutions per day: | 15.35744764 |
| mean anomaly at epoch: | 214.9221° |
| orbit number at epoch: | 3778 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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