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 68414U 26145.29768389 +.00000000 +00000-0 +86033-4 0 00000
2 68414 84.9669 242.2926 0025099 338.2933 21.7224 14.88582232 01
| Epoch (UTC): | 25 May 2026 07:08:39 |
| Eccentricity: | 0.0025099 |
| inclination: | 84.9669° |
| perigee height: | 585 km |
| apogee height: | 620 km |
| right ascension of ascending node: | 242.2926° |
| argument of perigee: | 338.2933° |
| revolutions per day: | 14.88582232 |
| mean anomaly at epoch: | 21.7224° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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