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 39444U 26145.38334711 +.00000000 +00000-0 +42758-3 0 00004
2 39444 97.8264 116.3600 0034467 282.1903 77.5466 15.09155971 06
| Epoch (UTC): | 25 May 2026 09:12:01 |
| Eccentricity: | 0.0034467 |
| inclination: | 97.8264° |
| perigee height: | 515 km |
| apogee height: | 563 km |
| right ascension of ascending node: | 116.3600° |
| argument of perigee: | 282.1903° |
| revolutions per day: | 15.09155971 |
| mean anomaly at epoch: | 77.5466° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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