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 68149U 26145.51099508 +.00000000 +00000-0 +68908-3 0 00000
2 68149 97.2865 167.2164 0000041 11.4140 348.7103 15.33456946 02
| Epoch (UTC): | 25 May 2026 12:15:49 |
| Eccentricity: | 0.0000041 |
| inclination: | 97.2865° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 167.2164° |
| argument of perigee: | 11.4140° |
| revolutions per day: | 15.33456946 |
| mean anomaly at epoch: | 348.7103° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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