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 18527U 26088.18542975 +.00000000 +00000-0 +21188-3 0 00004
2 18527 70.9953 81.0449 0193643 22.5138 338.4317 13.75793028 05
| Epoch (UTC): | 29 March 2026 04:27:01 |
| Eccentricity: | 0.0193643 |
| inclination: | 70.9953° |
| perigee height: | 836 km |
| apogee height: | 1121 km |
| right ascension of ascending node: | 81.0449° |
| argument of perigee: | 22.5138° |
| revolutions per day: | 13.75793028 |
| mean anomaly at epoch: | 338.4317° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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