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 57970U 26145.38152095 +.00000000 +00000-0 +30696-4 0 00000
2 57970 43.0048 117.4356 0001689 279.0428 81.0232 15.27577768 03
| Epoch (UTC): | 25 May 2026 09:09:23 |
| Eccentricity: | 0.0001689 |
| inclination: | 43.0048° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 117.4356° |
| argument of perigee: | 279.0428° |
| revolutions per day: | 15.27577768 |
| mean anomaly at epoch: | 81.0232° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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