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 64458U 26145.58335647 +.00000000 +00000-0 -13470-3 0 00008
2 64458 53.1579 91.1473 0001228 91.6832 98.6983 15.30194290 03
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001228 |
| inclination: | 53.1579° |
| perigee height: | 474 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 91.1473° |
| argument of perigee: | 91.6832° |
| revolutions per day: | 15.30194290 |
| mean anomaly at epoch: | 98.6983° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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