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 61750U 26145.61056709 +.00000000 +00000-0 +54358-3 0 00002
2 61750 97.2998 20.8744 0007032 27.9279 332.2351 15.53406617 05
| Epoch (UTC): | 25 May 2026 14:39:12 |
| Eccentricity: | 0.0007032 |
| inclination: | 97.2998° |
| perigee height: | 402 km |
| apogee height: | 412 km |
| right ascension of ascending node: | 20.8744° |
| argument of perigee: | 27.9279° |
| revolutions per day: | 15.53406617 |
| mean anomaly at epoch: | 332.2351° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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