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 26072.98053594 +.00000000 +00000-0 +13045-3 0 00008
2 04159 69.9611 63.9400 0111949 77.4173 283.9413 13.72895403 01
| Epoch (UTC): | 13 March 2026 23:31:58 |
| Eccentricity: | 0.0111949 |
| inclination: | 69.9611° |
| perigee height: | 907 km |
| apogee height: | 1072 km |
| right ascension of ascending node: | 63.9400° |
| argument of perigee: | 77.4173° |
| revolutions per day: | 13.72895403 |
| mean anomaly at epoch: | 283.9413° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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