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 68213U 26145.40722580 +.00000000 +00000-0 +37539-3 0 00009
2 68213 97.2868 20.8287 0001466 95.1240 265.0170 15.33449765 05
| Epoch (UTC): | 25 May 2026 09:46:24 |
| Eccentricity: | 0.0001466 |
| inclination: | 97.2868° |
| perigee height: | 465 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 20.8287° |
| argument of perigee: | 95.1240° |
| revolutions per day: | 15.33449765 |
| mean anomaly at epoch: | 265.0170° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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