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 00012U 26140.76618705 +.00000000 +00000-0 +50072-4 0 00007
2 00012 32.9089 321.8569 1646992 319.9636 29.0223 11.48609568 00
| Epoch (UTC): | 20 May 2026 18:23:18 |
| Eccentricity: | 0.1646992 |
| inclination: | 32.9089° |
| perigee height: | 553 km |
| apogee height: | 3286 km |
| right ascension of ascending node: | 321.8569° |
| argument of perigee: | 319.9636° |
| revolutions per day: | 11.48609568 |
| mean anomaly at epoch: | 29.0223° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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