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 04071U 26074.82452696 +.00000000 +00000-0 +99451-4 0 00008
2 04071 74.0467 116.6204 0014046 345.8382 14.2391 14.66587138 09
| Epoch (UTC): | 15 March 2026 19:47:19 |
| Eccentricity: | 0.0014046 |
| inclination: | 74.0467° |
| perigee height: | 662 km |
| apogee height: | 682 km |
| right ascension of ascending node: | 116.6204° |
| argument of perigee: | 345.8382° |
| revolutions per day: | 14.66587138 |
| mean anomaly at epoch: | 14.2391° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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