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 60077U 26145.49508102 +.00000000 +00000-0 -12935-5 0 00006
2 60077 53.1611 1.3399 0001036 94.4353 265.6768 15.34390736 03
| Epoch (UTC): | 25 May 2026 11:52:55 |
| Eccentricity: | 0.0001036 |
| inclination: | 53.1611° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 1.3399° |
| argument of perigee: | 94.4353° |
| revolutions per day: | 15.34390736 |
| mean anomaly at epoch: | 265.6768° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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