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 20453U 90008B 25318.74997550 .00035915 00000-0 61572-3 0 9993
2 20453 35.6069 200.9160 0117629 283.3097 75.4541 15.42699894908304
| Epoch (UTC): | 14 November 2025 17:59:57 |
| Eccentricity: | 0.0117629 |
| inclination: | 35.6069° |
| perigee height: | 358 km |
| apogee height: | 518 km |
| right ascension of ascending node: | 200.9160° |
| argument of perigee: | 283.3097° |
| revolutions per day: | 15.42699894 |
| mean anomaly at epoch: | 75.4541° |
| orbit number at epoch: | 90830 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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