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 62876U 26145.60166774 +.00000000 +00000-0 +00000-0 0 00007
2 62876 0.0142 316.4398 0002381 109.7341 124.1317 1.00271172 01
| Epoch (UTC): | 25 May 2026 14:26:24 |
| Eccentricity: | 0.0002381 |
| inclination: | 0.0142° |
| perigee height: | 35777 km |
| apogee height: | 35797 km |
| right ascension of ascending node: | 316.4398° |
| argument of perigee: | 109.7341° |
| revolutions per day: | 1.00271172 |
| mean anomaly at epoch: | 124.1317° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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