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 47303U 26145.62336741 +.00000000 +00000-0 +12769-3 0 00008
2 47303 98.0563 35.2735 0000859 289.4000 70.7110 14.64996171 04
| Epoch (UTC): | 25 May 2026 14:57:38 |
| Eccentricity: | 0.0000859 |
| inclination: | 98.0563° |
| perigee height: | 676 km |
| apogee height: | 678 km |
| right ascension of ascending node: | 35.2735° |
| argument of perigee: | 289.4000° |
| revolutions per day: | 14.64996171 |
| mean anomaly at epoch: | 70.7110° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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