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 28207U 26086.63453588 +.00000000 +00000-0 +29447-2 0 00004
2 28207 100.2868 141.5343 0041449 337.3142 174.6880 13.74509428 09
| Epoch (UTC): | 27 March 2026 15:13:43 |
| Eccentricity: | 0.0041449 |
| inclination: | 100.2868° |
| perigee height: | 953 km |
| apogee height: | 1014 km |
| right ascension of ascending node: | 141.5343° |
| argument of perigee: | 337.3142° |
| revolutions per day: | 13.74509428 |
| mean anomaly at epoch: | 174.6880° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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