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 68380U 26145.64421296 +.00000000 +00000-0 +11928-2 0 00003
2 68380 97.2853 289.5078 0000734 327.4146 32.7075 15.79139682 06
| Epoch (UTC): | 25 May 2026 15:27:40 |
| Eccentricity: | 0.0000734 |
| inclination: | 97.2853° |
| perigee height: | 332 km |
| apogee height: | 333 km |
| right ascension of ascending node: | 289.5078° |
| argument of perigee: | 327.4146° |
| revolutions per day: | 15.79139682 |
| mean anomaly at epoch: | 32.7075° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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