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 68551U 26145.32179374 +.00000000 +00000-0 +79917-3 0 00008
2 68551 53.1600 6.1985 0001104 86.7657 273.3472 15.34409323 08
| Epoch (UTC): | 25 May 2026 07:43:22 |
| Eccentricity: | 0.0001104 |
| inclination: | 53.1600° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 6.1985° |
| argument of perigee: | 86.7657° |
| revolutions per day: | 15.34409323 |
| mean anomaly at epoch: | 273.3472° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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