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 51061U 26145.60739440 +.00000000 +00000-0 +58242-3 0 00001
2 51061 97.3008 219.0982 0005862 63.3462 296.8387 15.45955057 07
| Epoch (UTC): | 25 May 2026 14:34:38 |
| Eccentricity: | 0.0005862 |
| inclination: | 97.3008° |
| perigee height: | 425 km |
| apogee height: | 433 km |
| right ascension of ascending node: | 219.0982° |
| argument of perigee: | 63.3462° |
| revolutions per day: | 15.45955057 |
| mean anomaly at epoch: | 296.8387° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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