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 68509U 26145.22548417 +.00000000 +00000-0 +68992-3 0 00009
2 68509 53.1610 132.2907 0000550 41.5844 318.5201 15.34399271 00
| Epoch (UTC): | 25 May 2026 05:24:41 |
| Eccentricity: | 0.0000550 |
| inclination: | 53.1610° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 132.2907° |
| argument of perigee: | 41.5844° |
| revolutions per day: | 15.34399271 |
| mean anomaly at epoch: | 318.5201° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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