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 39679U 26105.49129742 +.00000000 +00000-0 +18039-3 0 00003
2 39679 51.6056 157.5649 0093274 237.4932 121.7013 15.40466942 07
| Epoch (UTC): | 15 April 2026 11:47:28 |
| Eccentricity: | 0.0093274 |
| inclination: | 51.6056° |
| perigee height: | 381 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 157.5649° |
| argument of perigee: | 237.4932° |
| revolutions per day: | 15.40466942 |
| mean anomaly at epoch: | 121.7013° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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