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 58887U 26145.49853346 +.00000000 +00000-0 +37836-5 0 00001
2 58887 53.1620 325.4558 0000973 89.5805 270.5309 15.34389268 06
| Epoch (UTC): | 25 May 2026 11:57:53 |
| Eccentricity: | 0.0000973 |
| inclination: | 53.1620° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 325.4558° |
| argument of perigee: | 89.5805° |
| revolutions per day: | 15.34389268 |
| mean anomaly at epoch: | 270.5309° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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