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 68381U 26145.37380968 +.00000000 +00000-0 +70498-3 0 00002
2 68381 97.2866 287.8796 0001511 74.9873 285.1537 15.33456725 01
| Epoch (UTC): | 25 May 2026 08:58:17 |
| Eccentricity: | 0.0001511 |
| inclination: | 97.2866° |
| perigee height: | 464 km |
| apogee height: | 467 km |
| right ascension of ascending node: | 287.8796° |
| argument of perigee: | 74.9873° |
| revolutions per day: | 15.33456725 |
| mean anomaly at epoch: | 285.1537° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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