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 26046.07773450 +.00000000 +00000-0 +32774-3 0 00003
2 00012 32.9008 295.5890 1646803 178.4840 182.1597 11.48534804 06
| Epoch (UTC): | 15 February 2026 01:51:56 |
| Eccentricity: | 0.1646803 |
| inclination: | 32.9008° |
| perigee height: | 553 km |
| apogee height: | 3286 km |
| right ascension of ascending node: | 295.5890° |
| argument of perigee: | 178.4840° |
| revolutions per day: | 11.48534804 |
| mean anomaly at epoch: | 182.1597° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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