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 60199U 26145.50901579 +.00000000 +00000-0 +54971-4 0 00002
2 60199 53.1622 325.2137 0001164 77.7028 282.4104 15.34390925 04
| Epoch (UTC): | 25 May 2026 12:12:58 |
| Eccentricity: | 0.0001164 |
| inclination: | 53.1622° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 325.2137° |
| argument of perigee: | 77.7028° |
| revolutions per day: | 15.34390925 |
| mean anomaly at epoch: | 282.4104° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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