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 60917U 26145.40723203 +.00000000 +00000-0 +55645-4 0 00004
2 60917 53.1612 287.2944 0001021 78.9662 281.1453 15.30196331 07
| Epoch (UTC): | 25 May 2026 09:46:24 |
| Eccentricity: | 0.0001021 |
| inclination: | 53.1612° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 287.2944° |
| argument of perigee: | 78.9662° |
| revolutions per day: | 15.30196331 |
| mean anomaly at epoch: | 281.1453° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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