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 62636U 26145.19156630 +.00000000 +00000-0 +18123-2 0 00002
2 62636 97.3880 229.0138 0001742 143.4896 216.6474 15.48334949 04
| Epoch (UTC): | 25 May 2026 04:35:51 |
| Eccentricity: | 0.0001742 |
| inclination: | 97.3880° |
| perigee height: | 420 km |
| apogee height: | 423 km |
| right ascension of ascending node: | 229.0138° |
| argument of perigee: | 143.4896° |
| revolutions per day: | 15.48334949 |
| mean anomaly at epoch: | 216.6474° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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