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 26144.95716844 +.00000000 +00000-0 +00000-0 0 00000
2 40129 48.9181 273.4734 1672209 179.2149 181.1057 1.85520586 02
| Epoch (UTC): | 24 May 2026 22:58:19 |
| Eccentricity: | 0.1672209 |
| inclination: | 48.9181° |
| perigee height: | 16921 km |
| apogee height: | 26278 km |
| right ascension of ascending node: | 273.4734° |
| argument of perigee: | 179.2149° |
| revolutions per day: | 1.85520586 |
| mean anomaly at epoch: | 181.1057° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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