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 26037.12480884 +.00000000 +00000-0 +46997-3 0 00007
2 00012 32.9006 327.1455 1646733 131.0607 244.4404 11.48523469 05
| Epoch (UTC): | 06 February 2026 02:59:43 |
| Eccentricity: | 0.1646733 |
| inclination: | 32.9006° |
| perigee height: | 553 km |
| apogee height: | 3286 km |
| right ascension of ascending node: | 327.1455° |
| argument of perigee: | 131.0607° |
| revolutions per day: | 11.48523469 |
| mean anomaly at epoch: | 244.4404° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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