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 25023U 26158.73546604 +.00000000 +00000-0 +28932-2 0 00008
2 25023 7.9288 340.9154 6494626 150.6422 230.4618 3.10940881 09
| Epoch (UTC): | 07 June 2026 17:39:04 |
| Eccentricity: | 0.6494626 |
| inclination: | 7.9288° |
| perigee height: | 572 km |
| apogee height: | 26328 km |
| right ascension of ascending node: | 340.9154° |
| argument of perigee: | 150.6422° |
| revolutions per day: | 3.10940881 |
| mean anomaly at epoch: | 230.4618° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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