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 68725U 26145.13129163 +.00000000 +00000-0 +59565-3 0 00008
2 68725 53.1585 39.9502 0000909 95.6224 264.4889 15.49341894 00
| Epoch (UTC): | 25 May 2026 03:09:03 |
| Eccentricity: | 0.0000909 |
| inclination: | 53.1585° |
| perigee height: | 418 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 39.9502° |
| argument of perigee: | 95.6224° |
| revolutions per day: | 15.49341894 |
| mean anomaly at epoch: | 264.4889° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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