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 56204U 26145.50428712 +.00000000 +00000-0 +25099-3 0 00005
2 56204 97.3069 55.0096 0008369 113.6194 246.5938 15.52183401 06
| Epoch (UTC): | 25 May 2026 12:06:10 |
| Eccentricity: | 0.0008369 |
| inclination: | 97.3069° |
| perigee height: | 405 km |
| apogee height: | 416 km |
| right ascension of ascending node: | 55.0096° |
| argument of perigee: | 113.6194° |
| revolutions per day: | 15.52183401 |
| mean anomaly at epoch: | 246.5938° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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