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 23180U 26159.15548316 +.00000000 +00000-0 -32349-5 0 00000
2 23180 82.9473 11.4186 0029594 34.3628 84.4779 13.78302562 01
| Epoch (UTC): | 08 June 2026 03:43:53 |
| Eccentricity: | 0.0029594 |
| inclination: | 82.9473° |
| perigee height: | 948 km |
| apogee height: | 992 km |
| right ascension of ascending node: | 11.4186° |
| argument of perigee: | 34.3628° |
| revolutions per day: | 13.78302562 |
| mean anomaly at epoch: | 84.4779° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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