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 68624U 26145.58335647 +.00000000 +00000-0 -33666-1 0 00004
2 68624 97.2845 345.0512 0001461 84.2159 316.7363 15.52686641 07
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001461 |
| inclination: | 97.2845° |
| perigee height: | 408 km |
| apogee height: | 410 km |
| right ascension of ascending node: | 345.0512° |
| argument of perigee: | 84.2159° |
| revolutions per day: | 15.52686641 |
| mean anomaly at epoch: | 316.7363° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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