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 62631U 26145.50855531 +.00000000 +00000-0 +10040-4 0 00000
2 62631 97.3070 236.4030 0001275 48.7850 311.3506 15.40603319 02
| Epoch (UTC): | 25 May 2026 12:12:19 |
| Eccentricity: | 0.0001275 |
| inclination: | 97.3070° |
| perigee height: | 443 km |
| apogee height: | 445 km |
| right ascension of ascending node: | 236.4030° |
| argument of perigee: | 48.7850° |
| revolutions per day: | 15.40603319 |
| mean anomaly at epoch: | 311.3506° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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