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 26038.08106419 +.00000000 +00000-0 +47184-3 0 00001
2 00012 32.9005 323.7753 1646710 136.1253 238.2569 11.48524968 03
| Epoch (UTC): | 07 February 2026 01:56:43 |
| Eccentricity: | 0.1646710 |
| inclination: | 32.9005° |
| perigee height: | 553 km |
| apogee height: | 3286 km |
| right ascension of ascending node: | 323.7753° |
| argument of perigee: | 136.1253° |
| revolutions per day: | 11.48524968 |
| mean anomaly at epoch: | 238.2569° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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