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 26046.90762093 +.00000000 +00000-0 +13283-3 0 00008
2 00029 48.3768 240.9484 0021906 106.9309 253.4008 14.78580891 09
| Epoch (UTC): | 15 February 2026 21:46:58 |
| Eccentricity: | 0.0021906 |
| inclination: | 48.3768° |
| perigee height: | 618 km |
| apogee height: | 649 km |
| right ascension of ascending node: | 240.9484° |
| argument of perigee: | 106.9309° |
| revolutions per day: | 14.78580891 |
| mean anomaly at epoch: | 253.4008° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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