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 57369U 26145.53681345 +.00000000 +00000-0 +70635-4 0 00001
2 57369 43.0025 167.5470 0001308 254.0416 106.0292 15.27546407 01
| Epoch (UTC): | 25 May 2026 12:53:00 |
| Eccentricity: | 0.0001308 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 167.5470° |
| argument of perigee: | 254.0416° |
| revolutions per day: | 15.27546407 |
| mean anomaly at epoch: | 106.0292° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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