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 48029U 26145.61331782 +.00000000 +00000-0 +11320-2 0 00004
2 48029 53.1169 327.9671 0003223 262.3256 97.7389 15.53248142 09
| Epoch (UTC): | 25 May 2026 14:43:10 |
| Eccentricity: | 0.0003223 |
| inclination: | 53.1169° |
| perigee height: | 405 km |
| apogee height: | 409 km |
| right ascension of ascending node: | 327.9671° |
| argument of perigee: | 262.3256° |
| revolutions per day: | 15.53248142 |
| mean anomaly at epoch: | 97.7389° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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