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 61014U 26145.34031852 +.00000000 +00000-0 +29329-3 0 00007
2 61014 49.9969 99.9041 0003090 344.8642 15.2204 14.83154799 00
| Epoch (UTC): | 25 May 2026 08:10:03 |
| Eccentricity: | 0.0003090 |
| inclination: | 49.9969° |
| perigee height: | 617 km |
| apogee height: | 622 km |
| right ascension of ascending node: | 99.9041° |
| argument of perigee: | 344.8642° |
| revolutions per day: | 14.83154799 |
| mean anomaly at epoch: | 15.2204° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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