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 26154.73167875 +.00000000 +00000-0 +51139-3 0 00001
2 39444 97.8276 125.8984 0034698 248.4796 111.2732 15.09317269 02
| Epoch (UTC): | 03 June 2026 17:33:37 |
| Eccentricity: | 0.0034698 |
| inclination: | 97.8276° |
| perigee height: | 514 km |
| apogee height: | 562 km |
| right ascension of ascending node: | 125.8984° |
| argument of perigee: | 248.4796° |
| revolutions per day: | 15.09317269 |
| mean anomaly at epoch: | 111.2732° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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