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 04139U 26069.11421417 +.00000000 +00000-0 +14048-3 0 00004
2 04139 74.0295 104.2233 0003582 107.5239 252.6322 14.66475862 07
| Epoch (UTC): | 10 March 2026 02:44:28 |
| Eccentricity: | 0.0003582 |
| inclination: | 74.0295° |
| perigee height: | 670 km |
| apogee height: | 675 km |
| right ascension of ascending node: | 104.2233° |
| argument of perigee: | 107.5239° |
| revolutions per day: | 14.66475862 |
| mean anomaly at epoch: | 252.6322° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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