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 62209U 26145.17421219 +.00000000 +00000-0 +48613-3 0 00002
2 62209 42.9954 199.1982 0000325 4.7305 355.3550 15.27596224 01
| Epoch (UTC): | 25 May 2026 04:10:51 |
| Eccentricity: | 0.0000325 |
| inclination: | 42.9954° |
| perigee height: | 483 km |
| apogee height: | 483 km |
| right ascension of ascending node: | 199.1982° |
| argument of perigee: | 4.7305° |
| revolutions per day: | 15.27596224 |
| mean anomaly at epoch: | 355.3550° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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