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 08039U 26088.16855463 +.00000000 +00000-0 -13568-4 0 00003
2 08039 81.2984 149.4421 0025150 57.3069 303.0522 14.09317652 05
| Epoch (UTC): | 29 March 2026 04:02:43 |
| Eccentricity: | 0.0025150 |
| inclination: | 81.2984° |
| perigee height: | 843 km |
| apogee height: | 880 km |
| right ascension of ascending node: | 149.4421° |
| argument of perigee: | 57.3069° |
| revolutions per day: | 14.09317652 |
| mean anomaly at epoch: | 303.0522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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