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 60109U 26145.12200757 +.00000000 +00000-0 +68352-4 0 00009
2 60109 53.1612 41.7492 0001255 78.6808 281.4334 15.30196988 08
| Epoch (UTC): | 25 May 2026 02:55:41 |
| Eccentricity: | 0.0001255 |
| inclination: | 53.1612° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 41.7492° |
| argument of perigee: | 78.6808° |
| revolutions per day: | 15.30196988 |
| mean anomaly at epoch: | 281.4334° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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