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 39484U 26104.17834965 +.00000000 +00000-0 +54456-3 0 00004
2 39484 82.4902 209.9245 0020579 232.3215 127.5999 12.42878803 02
| Epoch (UTC): | 14 April 2026 04:16:49 |
| Eccentricity: | 0.0020579 |
| inclination: | 82.4902° |
| perigee height: | 1478 km |
| apogee height: | 1511 km |
| right ascension of ascending node: | 209.9245° |
| argument of perigee: | 232.3215° |
| revolutions per day: | 12.42878803 |
| mean anomaly at epoch: | 127.5999° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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