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 42070U 26083.18239207 +.00000000 +00000-0 +00000-0 0 00007
2 42070 0.0186 165.4536 0001980 194.1008 137.8721 1.00271046 01
| Epoch (UTC): | 24 March 2026 04:22:38 |
| Eccentricity: | 0.0001980 |
| inclination: | 0.0186° |
| perigee height: | 35778 km |
| apogee height: | 35795 km |
| right ascension of ascending node: | 165.4536° |
| argument of perigee: | 194.1008° |
| revolutions per day: | 1.00271046 |
| mean anomaly at epoch: | 137.8721° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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