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 68702U 26145.13207669 +.00000000 +00000-0 +92634-3 0 00005
2 68702 53.1598 39.9592 0000793 116.3408 243.7682 15.49323883 03
| Epoch (UTC): | 25 May 2026 03:10:11 |
| Eccentricity: | 0.0000793 |
| inclination: | 53.1598° |
| perigee height: | 418 km |
| apogee height: | 419 km |
| right ascension of ascending node: | 39.9592° |
| argument of perigee: | 116.3408° |
| revolutions per day: | 15.49323883 |
| mean anomaly at epoch: | 243.7682° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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