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 68708U 26145.58335647 +.00000000 +00000-0 -48365-1 0 00009
2 68708 53.1602 37.2263 0001129 116.6752 164.4409 15.43353468 02
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001129 |
| inclination: | 53.1602° |
| perigee height: | 435 km |
| apogee height: | 437 km |
| right ascension of ascending node: | 37.2263° |
| argument of perigee: | 116.6752° |
| revolutions per day: | 15.43353468 |
| mean anomaly at epoch: | 164.4409° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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