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 59015U 26145.52787352 +.00000000 +00000-0 -35223-4 0 00000
2 59015 53.1612 81.4922 0001477 97.2204 262.8965 15.30178370 02
| Epoch (UTC): | 25 May 2026 12:40:08 |
| Eccentricity: | 0.0001477 |
| inclination: | 53.1612° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 81.4922° |
| argument of perigee: | 97.2204° |
| revolutions per day: | 15.30178370 |
| mean anomaly at epoch: | 262.8965° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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