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 61846U 26145.46807912 +.00000000 +00000-0 +48170-5 0 00008
2 61846 43.0020 153.6848 0001536 276.4491 83.6186 15.27574858 03
| Epoch (UTC): | 25 May 2026 11:14:02 |
| Eccentricity: | 0.0001536 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 153.6848° |
| argument of perigee: | 276.4491° |
| revolutions per day: | 15.27574858 |
| mean anomaly at epoch: | 83.6186° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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