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 68220U 26145.38547602 +.00000000 +00000-0 +52074-3 0 00005
2 68220 97.2865 20.8564 0001908 90.6896 269.4565 15.33444542 00
| Epoch (UTC): | 25 May 2026 09:15:05 |
| Eccentricity: | 0.0001908 |
| inclination: | 97.2865° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 20.8564° |
| argument of perigee: | 90.6896° |
| revolutions per day: | 15.33444542 |
| mean anomaly at epoch: | 269.4565° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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