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 09663U 26087.98887670 +.00000000 +00000-0 +52773-5 0 00002
2 09663 81.2688 184.4938 0006400 221.8531 138.2147 14.02790572 01
| Epoch (UTC): | 28 March 2026 23:43:58 |
| Eccentricity: | 0.0006400 |
| inclination: | 81.2688° |
| perigee height: | 880 km |
| apogee height: | 889 km |
| right ascension of ascending node: | 184.4938° |
| argument of perigee: | 221.8531° |
| revolutions per day: | 14.02790572 |
| mean anomaly at epoch: | 138.2147° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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