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 26022.86059794 +.00000000 +00000-0 +22975-3 0 00008
2 04139 74.0297 193.4117 0005698 214.5315 145.5485 14.66389875 02
| Epoch (UTC): | 22 January 2026 20:39:15 |
| Eccentricity: | 0.0005698 |
| inclination: | 74.0297° |
| perigee height: | 669 km |
| apogee height: | 677 km |
| right ascension of ascending node: | 193.4117° |
| argument of perigee: | 214.5315° |
| revolutions per day: | 14.66389875 |
| mean anomaly at epoch: | 145.5485° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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