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 is defined by the following mean orbital elements,
1 04382U 26088.14627588 +.00000000 +00000-0 +23789-3 0 00007
2 04382 68.4256 225.1273 1028118 52.3833 316.6126 13.14253228 03
| Epoch (UTC): | 29 March 2026 03:30:38 |
| Eccentricity: | 0.1028118 |
| inclination: | 68.4256° |
| perigee height: | 427 km |
| apogee height: | 1987 km |
| right ascension of ascending node: | 225.1273° |
| argument of perigee: | 52.3833° |
| revolutions per day: | 13.14253228 |
| mean anomaly at epoch: | 316.6126° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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