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 42063U 26154.29138377 +.00000000 +00000-0 +14986-4 0 00008
2 42063 98.5693 229.2612 0001204 86.1561 273.9760 14.30812463 01
| Epoch (UTC): | 03 June 2026 06:59:35 |
| Eccentricity: | 0.0001204 |
| inclination: | 98.5693° |
| perigee height: | 788 km |
| apogee height: | 790 km |
| right ascension of ascending node: | 229.2612° |
| argument of perigee: | 86.1561° |
| revolutions per day: | 14.30812463 |
| mean anomaly at epoch: | 273.9760° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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