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 61775U 26145.53334176 +.00000000 +00000-0 +35599-3 0 00003
2 61775 97.3025 17.7655 0014925 9.4729 350.6797 15.43594190 05
| Epoch (UTC): | 25 May 2026 12:48:00 |
| Eccentricity: | 0.0014925 |
| inclination: | 97.3025° |
| perigee height: | 425 km |
| apogee height: | 446 km |
| right ascension of ascending node: | 17.7655° |
| argument of perigee: | 9.4729° |
| revolutions per day: | 15.43594190 |
| mean anomaly at epoch: | 350.6797° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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