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 18187U 26074.93839337 +.00000000 +00000-0 +33601-4 0 00009
2 18187 65.0101 289.2058 0014587 279.0350 80.9084 14.31503965 01
| Epoch (UTC): | 15 March 2026 22:31:17 |
| Eccentricity: | 0.0014587 |
| inclination: | 65.0101° |
| perigee height: | 776 km |
| apogee height: | 797 km |
| right ascension of ascending node: | 289.2058° |
| argument of perigee: | 279.0350° |
| revolutions per day: | 14.31503965 |
| mean anomaly at epoch: | 80.9084° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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