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 62623U 26145.17871064 +.00000000 +00000-0 +34645-3 0 00009
2 62623 97.4027 227.4259 0005460 48.7968 311.3742 15.29364737 06
| Epoch (UTC): | 25 May 2026 04:17:20 |
| Eccentricity: | 0.0005460 |
| inclination: | 97.4027° |
| perigee height: | 474 km |
| apogee height: | 481 km |
| right ascension of ascending node: | 227.4259° |
| argument of perigee: | 48.7968° |
| revolutions per day: | 15.29364737 |
| mean anomaly at epoch: | 311.3742° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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