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 39013U 26145.59062618 +.00000000 +00000-0 +20572-3 0 00003
2 39013 63.3564 347.8801 0433990 26.2753 335.9597 13.45504249 07
| Epoch (UTC): | 25 May 2026 14:10:30 |
| Eccentricity: | 0.0433990 |
| inclination: | 63.3564° |
| perigee height: | 765 km |
| apogee height: | 1413 km |
| right ascension of ascending node: | 347.8801° |
| argument of perigee: | 26.2753° |
| revolutions per day: | 13.45504249 |
| mean anomaly at epoch: | 335.9597° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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