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 27819U 03023B 25350.98861941 .00000081 00000-0 69002-4 0 9996
2 27819 82.9481 249.1248 0047544 51.3632 319.5059 13.74512644130200
| Epoch (UTC): | 16 December 2025 23:43:36 |
| Eccentricity: | 0.0047544 |
| inclination: | 82.9481° |
| perigee height: | 948 km |
| apogee height: | 1018 km |
| right ascension of ascending node: | 249.1248° |
| argument of perigee: | 51.3632° |
| revolutions per day: | 13.74512644 |
| mean anomaly at epoch: | 319.5059° |
| orbit number at epoch: | 13020 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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