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 67848U 26145.53489373 +.00000000 +00000-0 +65618-3 0 00005
2 67848 43.0006 193.3174 0001924 266.7394 93.3237 15.27596916 07
| Epoch (UTC): | 25 May 2026 12:50:14 |
| Eccentricity: | 0.0001924 |
| inclination: | 43.0006° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 193.3174° |
| argument of perigee: | 266.7394° |
| revolutions per day: | 15.27596916 |
| mean anomaly at epoch: | 93.3237° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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