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 60377U 26145.47371696 +.00000000 +00000-0 +11846-4 0 00001
2 60377 53.1612 312.9400 0001185 78.9964 281.1170 15.30196447 00
| Epoch (UTC): | 25 May 2026 11:22:09 |
| Eccentricity: | 0.0001185 |
| inclination: | 53.1612° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 312.9400° |
| argument of perigee: | 78.9964° |
| revolutions per day: | 15.30196447 |
| mean anomaly at epoch: | 281.1170° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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