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 68727U 26145.11817080 +.00000000 +00000-0 +55987-3 0 00004
2 68727 53.1599 39.8655 0001153 83.1344 276.9796 15.49350391 09
| Epoch (UTC): | 25 May 2026 02:50:09 |
| Eccentricity: | 0.0001153 |
| inclination: | 53.1599° |
| perigee height: | 418 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 39.8655° |
| argument of perigee: | 83.1344° |
| revolutions per day: | 15.49350391 |
| mean anomaly at epoch: | 276.9796° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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