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 21903U 92012B 25197.96073027 .00000085 00000-0 72736-4 0 9999
2 21903 82.9380 156.9711 0043427 143.3289 278.4026 13.74729851672817
| Epoch (UTC): | 16 July 2025 23:03:27 |
| Eccentricity: | 0.0043427 |
| inclination: | 82.9380° |
| perigee height: | 950 km |
| apogee height: | 1014 km |
| right ascension of ascending node: | 156.9711° |
| argument of perigee: | 143.3289° |
| revolutions per day: | 13.74729851 |
| mean anomaly at epoch: | 278.4026° |
| orbit number at epoch: | 67281 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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