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 40129U 26144.41818597 +.00000000 +00000-0 +00000-0 0 00009
2 40129 48.9189 273.4954 1672128 179.1933 181.1360 1.85520556 08
| Epoch (UTC): | 24 May 2026 10:02:11 |
| Eccentricity: | 0.1672128 |
| inclination: | 48.9189° |
| perigee height: | 16921 km |
| apogee height: | 26277 km |
| right ascension of ascending node: | 273.4954° |
| argument of perigee: | 179.1933° |
| revolutions per day: | 1.85520556 |
| mean anomaly at epoch: | 181.1360° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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