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 67294U 26145.63571546 +.00000000 +00000-0 +39380-3 0 00002
2 67294 97.3948 221.0044 0010390 80.3198 279.9213 15.24555565 01
| Epoch (UTC): | 25 May 2026 15:15:25 |
| Eccentricity: | 0.0010390 |
| inclination: | 97.3948° |
| perigee height: | 485 km |
| apogee height: | 499 km |
| right ascension of ascending node: | 221.0044° |
| argument of perigee: | 80.3198° |
| revolutions per day: | 15.24555565 |
| mean anomaly at epoch: | 279.9213° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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