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 26032.05488177 +.00000000 +00000-0 +21266-3 0 00003
2 04382 68.4306 339.4997 1028366 103.1967 268.5716 13.14073379 06
| Epoch (UTC): | 01 February 2026 01:19:01 |
| Eccentricity: | 0.1028366 |
| inclination: | 68.4306° |
| perigee height: | 427 km |
| apogee height: | 1988 km |
| right ascension of ascending node: | 339.4997° |
| argument of perigee: | 103.1967° |
| revolutions per day: | 13.14073379 |
| mean anomaly at epoch: | 268.5716° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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