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 61752U 26145.60438058 +.00000000 +00000-0 +16519-3 0 00001
2 61752 97.3250 346.4199 0007088 133.9845 226.1964 14.97535072 04
| Epoch (UTC): | 25 May 2026 14:30:18 |
| Eccentricity: | 0.0007088 |
| inclination: | 97.3250° |
| perigee height: | 570 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 346.4199° |
| argument of perigee: | 133.9845° |
| revolutions per day: | 14.97535072 |
| mean anomaly at epoch: | 226.1964° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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