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 57602U 26144.96176147 +.00000000 +00000-0 -26565-4 0 00000
2 57602 43.0042 10.6306 0002201 253.5464 106.5146 15.27588987 08
| Epoch (UTC): | 24 May 2026 23:04:56 |
| Eccentricity: | 0.0002201 |
| inclination: | 43.0042° |
| perigee height: | 482 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 10.6306° |
| argument of perigee: | 253.5464° |
| revolutions per day: | 15.27588987 |
| mean anomaly at epoch: | 106.5146° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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