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 68254U 26145.13933475 +.00000000 +00000-0 +11276-2 0 00000
2 68254 53.1583 297.7261 0001291 92.1817 267.9340 15.49362342 07
| Epoch (UTC): | 25 May 2026 03:20:38 |
| Eccentricity: | 0.0001291 |
| inclination: | 53.1583° |
| perigee height: | 418 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 297.7261° |
| argument of perigee: | 92.1817° |
| revolutions per day: | 15.49362342 |
| mean anomaly at epoch: | 267.9340° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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