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 26019.26767149 +.00000000 +00000-0 +13258-3 0 00006
2 00029 48.3795 12.2586 0022589 345.9124 14.1157 14.78503657 02
| Epoch (UTC): | 19 January 2026 06:25:26 |
| Eccentricity: | 0.0022589 |
| inclination: | 48.3795° |
| perigee height: | 618 km |
| apogee height: | 650 km |
| right ascension of ascending node: | 12.2586° |
| argument of perigee: | 345.9124° |
| revolutions per day: | 14.78503657 |
| mean anomaly at epoch: | 14.1157° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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