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 55244U 26145.63212785 +.00000000 +00000-0 +27084-3 0 00009
2 55244 43.1966 247.6211 0018157 233.0969 126.8218 15.16961444 07
| Epoch (UTC): | 25 May 2026 15:10:15 |
| Eccentricity: | 0.0018157 |
| inclination: | 43.1966° |
| perigee height: | 503 km |
| apogee height: | 528 km |
| right ascension of ascending node: | 247.6211° |
| argument of perigee: | 233.0969° |
| revolutions per day: | 15.16961444 |
| mean anomaly at epoch: | 126.8218° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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