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 61046U 26145.13433742 +.00000000 +00000-0 +10191-2 0 00009
2 61046 52.9733 55.3805 0009842 54.4943 305.6968 15.20720001 01
| Epoch (UTC): | 25 May 2026 03:13:26 |
| Eccentricity: | 0.0009842 |
| inclination: | 52.9733° |
| perigee height: | 497 km |
| apogee height: | 510 km |
| right ascension of ascending node: | 55.3805° |
| argument of perigee: | 54.4943° |
| revolutions per day: | 15.20720001 |
| mean anomaly at epoch: | 305.6968° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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