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 56202U 26145.67636792 +.00000000 +00000-0 +55023-3 0 00000
2 56202 97.3077 55.7878 0014376 133.4305 226.8145 15.48053296 01
| Epoch (UTC): | 25 May 2026 16:13:58 |
| Eccentricity: | 0.0014376 |
| inclination: | 97.3077° |
| perigee height: | 413 km |
| apogee height: | 432 km |
| right ascension of ascending node: | 55.7878° |
| argument of perigee: | 133.4305° |
| revolutions per day: | 15.48053296 |
| mean anomaly at epoch: | 226.8145° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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