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 68520U 26145.36838065 +.00000000 +00000-0 +52158-3 0 00005
2 68520 53.1601 131.7661 0001299 85.6225 274.4926 15.34394109 06
| Epoch (UTC): | 25 May 2026 08:50:28 |
| Eccentricity: | 0.0001299 |
| inclination: | 53.1601° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 131.7661° |
| argument of perigee: | 85.6225° |
| revolutions per day: | 15.34394109 |
| mean anomaly at epoch: | 274.4926° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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