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 67834U 26145.42452441 +.00000000 +00000-0 +15044-3 0 00002
2 67834 43.0011 193.3431 0001253 268.1546 91.9162 15.27567128 08
| Epoch (UTC): | 25 May 2026 10:11:18 |
| Eccentricity: | 0.0001253 |
| inclination: | 43.0011° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 193.3431° |
| argument of perigee: | 268.1546° |
| revolutions per day: | 15.27567128 |
| mean anomaly at epoch: | 91.9162° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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