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 26047.03379088 +.00000000 +00000-0 +38390-3 0 00009
2 00012 32.9012 292.2190 1646825 183.5490 175.1953 11.48536635 02
| Epoch (UTC): | 16 February 2026 00:48:39 |
| Eccentricity: | 0.1646825 |
| inclination: | 32.9012° |
| perigee height: | 553 km |
| apogee height: | 3286 km |
| right ascension of ascending node: | 292.2190° |
| argument of perigee: | 183.5490° |
| revolutions per day: | 11.48536635 |
| mean anomaly at epoch: | 175.1953° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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