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 00029U 26037.04120412 +.00000000 +00000-0 +15380-3 0 00006
2 00029 48.3784 287.8243 0021928 63.3354 296.9802 14.78561407 06
| Epoch (UTC): | 06 February 2026 00:59:20 |
| Eccentricity: | 0.0021928 |
| inclination: | 48.3784° |
| perigee height: | 618 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 287.8243° |
| argument of perigee: | 63.3354° |
| revolutions per day: | 14.78561407 |
| mean anomaly at epoch: | 296.9802° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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