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 68369U 26145.17870501 +.00000000 +00000-0 +24207-3 0 00000
2 68369 82.2965 37.7846 0014958 175.9491 184.1907 15.93702667 00
| Epoch (UTC): | 25 May 2026 04:17:20 |
| Eccentricity: | 0.0014958 |
| inclination: | 82.2965° |
| perigee height: | 282 km |
| apogee height: | 302 km |
| right ascension of ascending node: | 37.7846° |
| argument of perigee: | 175.9491° |
| revolutions per day: | 15.93702667 |
| mean anomaly at epoch: | 184.1907° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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