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 39971U 26086.40034575 +.00000000 +00000-0 +11867-2 0 00007
2 39971 82.4557 321.1375 0062550 299.2613 241.0914 13.90602423 05
| Epoch (UTC): | 27 March 2026 09:36:29 |
| Eccentricity: | 0.0062550 |
| inclination: | 82.4557° |
| perigee height: | 881 km |
| apogee height: | 972 km |
| right ascension of ascending node: | 321.1375° |
| argument of perigee: | 299.2613° |
| revolutions per day: | 13.90602423 |
| mean anomaly at epoch: | 241.0914° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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