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 55247U 26145.00782345 +.00000000 +00000-0 +00000-0 0 00003
2 55247 5.3265 64.3491 0008994 311.8035 201.2798 0.99053278 06
| Epoch (UTC): | 25 May 2026 00:11:15 |
| Eccentricity: | 0.0008994 |
| inclination: | 5.3265° |
| perigee height: | 36093 km |
| apogee height: | 36170 km |
| right ascension of ascending node: | 64.3491° |
| argument of perigee: | 311.8035° |
| revolutions per day: | 0.99053278 |
| mean anomaly at epoch: | 201.2798° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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