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 69013U 26145.57921203 +.00000000 +00000-0 +28518-3 0 00006
2 69013 97.4098 43.8228 0009298 97.9191 262.3100 15.20417877 05
| Epoch (UTC): | 25 May 2026 13:54:03 |
| Eccentricity: | 0.0009298 |
| inclination: | 97.4098° |
| perigee height: | 498 km |
| apogee height: | 511 km |
| right ascension of ascending node: | 43.8228° |
| argument of perigee: | 97.9191° |
| revolutions per day: | 15.20417877 |
| mean anomaly at epoch: | 262.3100° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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