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 68460U 26145.37206934 +.00000000 +00000-0 +53134-3 0 00008
2 68460 97.4481 104.0551 0007327 134.6423 225.5409 15.17322994 07
| Epoch (UTC): | 25 May 2026 08:55:46 |
| Eccentricity: | 0.0007327 |
| inclination: | 97.4481° |
| perigee height: | 509 km |
| apogee height: | 519 km |
| right ascension of ascending node: | 104.0551° |
| argument of perigee: | 134.6423° |
| revolutions per day: | 15.17322994 |
| mean anomaly at epoch: | 225.5409° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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