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 10517U 26072.94692199 +.00000000 +00000-0 +34021-3 0 00006
2 10517 28.6563 165.1263 0813974 156.1309 207.9273 13.47367599 01
| Epoch (UTC): | 13 March 2026 22:43:34 |
| Eccentricity: | 0.0813974 |
| inclination: | 28.6563° |
| perigee height: | 475 km |
| apogee height: | 1689 km |
| right ascension of ascending node: | 165.1263° |
| argument of perigee: | 156.1309° |
| revolutions per day: | 13.47367599 |
| mean anomaly at epoch: | 207.9273° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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