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 68261U 26145.06094150 +.00000000 +00000-0 +32072-3 0 00006
2 68261 51.6618 69.6677 0006643 73.9925 286.1785 15.23568436 07
| Epoch (UTC): | 25 May 2026 01:27:45 |
| Eccentricity: | 0.0006643 |
| inclination: | 51.6618° |
| perigee height: | 491 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 69.6677° |
| argument of perigee: | 73.9925° |
| revolutions per day: | 15.23568436 |
| mean anomaly at epoch: | 286.1785° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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