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 60395U 26145.56205959 +.00000000 +00000-0 +13175-3 0 00005
2 60395 88.9726 282.4517 0017016 94.1756 266.1340 13.51006782 06
| Epoch (UTC): | 25 May 2026 13:29:21 |
| Eccentricity: | 0.0017016 |
| inclination: | 88.9726° |
| perigee height: | 1056 km |
| apogee height: | 1081 km |
| right ascension of ascending node: | 282.4517° |
| argument of perigee: | 94.1756° |
| revolutions per day: | 13.51006782 |
| mean anomaly at epoch: | 266.1340° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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