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 41882U 26145.60823279 +.00000000 +00000-0 +00000-0 0 00001
2 41882 2.2681 80.5193 0008385 146.1917 359.0178 1.00264292 02
| Epoch (UTC): | 25 May 2026 14:35:51 |
| Eccentricity: | 0.0008385 |
| inclination: | 2.2681° |
| perigee height: | 35753 km |
| apogee height: | 35824 km |
| right ascension of ascending node: | 80.5193° |
| argument of perigee: | 146.1917° |
| revolutions per day: | 1.00264292 |
| mean anomaly at epoch: | 359.0178° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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