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 69037U 26145.58335647 +.00000000 +00000-0 -18301-1 0 00002
2 69037 97.2847 0.3651 0001346 84.1089 245.8292 15.69585031 08
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0001346 |
| inclination: | 97.2847° |
| perigee height: | 359 km |
| apogee height: | 361 km |
| right ascension of ascending node: | 0.3651° |
| argument of perigee: | 84.1089° |
| revolutions per day: | 15.69585031 |
| mean anomaly at epoch: | 245.8292° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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