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 61863U 26145.50903128 +.00000000 +00000-0 +26244-4 0 00005
2 61863 43.0027 164.3741 0001435 274.0884 85.9804 15.27577814 05
| Epoch (UTC): | 25 May 2026 12:13:00 |
| Eccentricity: | 0.0001435 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 164.3741° |
| argument of perigee: | 274.0884° |
| revolutions per day: | 15.27577814 |
| mean anomaly at epoch: | 85.9804° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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