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 68304U 26145.35301720 +.00000000 +00000-0 +10968-2 0 00009
2 68304 97.2842 271.6107 0001464 50.3207 309.8188 15.75241462 05
| Epoch (UTC): | 25 May 2026 08:28:20 |
| Eccentricity: | 0.0001464 |
| inclination: | 97.2842° |
| perigee height: | 343 km |
| apogee height: | 345 km |
| right ascension of ascending node: | 271.6107° |
| argument of perigee: | 50.3207° |
| revolutions per day: | 15.75241462 |
| mean anomaly at epoch: | 309.8188° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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