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 62273U 26144.90048990 +.00000000 +00000-0 +12588-2 0 00005
2 62273 42.9987 317.6485 0001703 237.6412 122.4291 15.70886581 01
| Epoch (UTC): | 24 May 2026 21:36:42 |
| Eccentricity: | 0.0001703 |
| inclination: | 42.9987° |
| perigee height: | 355 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 317.6485° |
| argument of perigee: | 237.6412° |
| revolutions per day: | 15.70886581 |
| mean anomaly at epoch: | 122.4291° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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