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 68001U 26145.22366927 +.00000000 +00000-0 +72639-3 0 00003
2 68001 43.0057 337.1142 0001345 260.1428 99.9272 15.27598381 00
| Epoch (UTC): | 25 May 2026 05:22:05 |
| Eccentricity: | 0.0001345 |
| inclination: | 43.0057° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 337.1142° |
| argument of perigee: | 260.1428° |
| revolutions per day: | 15.27598381 |
| mean anomaly at epoch: | 99.9272° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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