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 68367U 26145.18442184 +.00000000 +00000-0 +29437-3 0 00001
2 68367 82.2960 37.9630 0007409 176.1964 183.9363 15.84564234 06
| Epoch (UTC): | 25 May 2026 04:25:34 |
| Eccentricity: | 0.0007409 |
| inclination: | 82.2960° |
| perigee height: | 313 km |
| apogee height: | 323 km |
| right ascension of ascending node: | 37.9630° |
| argument of perigee: | 176.1964° |
| revolutions per day: | 15.84564234 |
| mean anomaly at epoch: | 183.9363° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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