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 60601U 26145.19271282 +.00000000 +00000-0 +33083-4 0 00007
2 60601 53.1623 311.0157 0001414 93.8514 266.2651 15.34390519 01
| Epoch (UTC): | 25 May 2026 04:37:30 |
| Eccentricity: | 0.0001414 |
| inclination: | 53.1623° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 311.0157° |
| argument of perigee: | 93.8514° |
| revolutions per day: | 15.34390519 |
| mean anomaly at epoch: | 266.2651° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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