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 62913U 26145.33029257 +.00000000 +00000-0 +12646-2 0 00004
2 62913 43.0058 245.8796 0005219 274.3686 85.6585 15.70903136 09
| Epoch (UTC): | 25 May 2026 07:55:37 |
| Eccentricity: | 0.0005219 |
| inclination: | 43.0058° |
| perigee height: | 353 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 245.8796° |
| argument of perigee: | 274.3686° |
| revolutions per day: | 15.70903136 |
| mean anomaly at epoch: | 85.6585° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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