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 04159U 26073.41767808 +.00000000 +00000-0 +13080-3 0 00006
2 04159 69.9612 63.0392 0111951 76.8605 284.4953 13.72895480 09
| Epoch (UTC): | 14 March 2026 10:01:27 |
| Eccentricity: | 0.0111951 |
| inclination: | 69.9612° |
| perigee height: | 907 km |
| apogee height: | 1072 km |
| right ascension of ascending node: | 63.0392° |
| argument of perigee: | 76.8605° |
| revolutions per day: | 13.72895480 |
| mean anomaly at epoch: | 284.4953° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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