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 60317U 26145.45528968 +.00000000 +00000-0 +17429-4 0 00002
2 60317 53.1606 300.4809 0001029 77.0275 283.0841 15.30198087 02
| Epoch (UTC): | 25 May 2026 10:55:37 |
| Eccentricity: | 0.0001029 |
| inclination: | 53.1606° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 300.4809° |
| argument of perigee: | 77.0275° |
| revolutions per day: | 15.30198087 |
| mean anomaly at epoch: | 283.0841° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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