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 68897U 26145.26768368 +.00000000 +00000-0 +10777-2 0 00009
2 68897 97.2851 340.9564 0001106 85.5288 274.6089 15.49203928 06
| Epoch (UTC): | 25 May 2026 06:25:27 |
| Eccentricity: | 0.0001106 |
| inclination: | 97.2851° |
| perigee height: | 418 km |
| apogee height: | 420 km |
| right ascension of ascending node: | 340.9564° |
| argument of perigee: | 85.5288° |
| revolutions per day: | 15.49203928 |
| mean anomaly at epoch: | 274.6089° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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