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 60379U 26145.59512381 +.00000000 +00000-0 +12402-3 0 00002
2 60379 88.9714 282.2742 0019595 102.0406 258.2943 13.51010642 09
| Epoch (UTC): | 25 May 2026 14:16:58 |
| Eccentricity: | 0.0019595 |
| inclination: | 88.9714° |
| perigee height: | 1054 km |
| apogee height: | 1083 km |
| right ascension of ascending node: | 282.2742° |
| argument of perigee: | 102.0406° |
| revolutions per day: | 13.51010642 |
| mean anomaly at epoch: | 258.2943° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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