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 68094U 26145.53421306 +.00000000 +00000-0 +65221-3 0 00001
2 68094 53.1576 180.8421 0001002 93.8295 266.2822 15.34401948 06
| Epoch (UTC): | 25 May 2026 12:49:16 |
| Eccentricity: | 0.0001002 |
| inclination: | 53.1576° |
| perigee height: | 462 km |
| apogee height: | 463 km |
| right ascension of ascending node: | 180.8421° |
| argument of perigee: | 93.8295° |
| revolutions per day: | 15.34401948 |
| mean anomaly at epoch: | 266.2822° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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