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 67117U 26145.23812520 +.00000000 +00000-0 +96285-3 0 00009
2 67117 43.0018 96.6596 0001295 270.2495 89.8208 15.27594727 01
| Epoch (UTC): | 25 May 2026 05:42:54 |
| Eccentricity: | 0.0001295 |
| inclination: | 43.0018° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 96.6596° |
| argument of perigee: | 270.2495° |
| revolutions per day: | 15.27594727 |
| mean anomaly at epoch: | 89.8208° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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