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 60094U 26145.42759551 +.00000000 +00000-0 -81770-5 0 00007
2 60094 53.1622 40.8098 0001281 87.1528 272.9619 15.30188676 03
| Epoch (UTC): | 25 May 2026 10:15:44 |
| Eccentricity: | 0.0001281 |
| inclination: | 53.1622° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 40.8098° |
| argument of perigee: | 87.1528° |
| revolutions per day: | 15.30188676 |
| mean anomaly at epoch: | 272.9619° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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