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 61982U 26145.26235406 +.00000000 +00000-0 +52304-3 0 00002
2 61982 43.0000 107.1316 0001283 271.9078 88.1626 15.27595086 01
| Epoch (UTC): | 25 May 2026 06:17:47 |
| Eccentricity: | 0.0001283 |
| inclination: | 43.0000° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 107.1316° |
| argument of perigee: | 271.9078° |
| revolutions per day: | 15.27595086 |
| mean anomaly at epoch: | 88.1626° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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