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 18025U 26140.19500668 +.00000000 +00000-0 +44515-3 0 00009
2 18025 63.2910 71.6903 0782387 102.9007 266.0539 13.90033467 06
| Epoch (UTC): | 20 May 2026 04:40:48 |
| Eccentricity: | 0.0782387 |
| inclination: | 63.2910° |
| perigee height: | 357 km |
| apogee height: | 1500 km |
| right ascension of ascending node: | 71.6903° |
| argument of perigee: | 102.9007° |
| revolutions per day: | 13.90033467 |
| mean anomaly at epoch: | 266.0539° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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