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 61704U 26145.32972345 +.00000000 +00000-0 +17425-3 0 00006
2 61704 53.1590 158.0808 0001224 85.0232 275.0910 15.34404070 04
| Epoch (UTC): | 25 May 2026 07:54:48 |
| Eccentricity: | 0.0001224 |
| inclination: | 53.1590° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 158.0808° |
| argument of perigee: | 85.0232° |
| revolutions per day: | 15.34404070 |
| mean anomaly at epoch: | 275.0910° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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