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 68266U 26145.50803155 +.00000000 +00000-0 +82550-3 0 00009
2 68266 53.1587 321.6390 0001180 115.7978 244.3147 15.35415952 06
| Epoch (UTC): | 25 May 2026 12:11:33 |
| Eccentricity: | 0.0001180 |
| inclination: | 53.1587° |
| perigee height: | 459 km |
| apogee height: | 460 km |
| right ascension of ascending node: | 321.6390° |
| argument of perigee: | 115.7978° |
| revolutions per day: | 15.35415952 |
| mean anomaly at epoch: | 244.3147° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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