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 28372U 26133.48914160 +.00000000 +00000-0 +48370-4 0 00009
2 28372 98.6316 143.2685 0043417 260.5191 99.1094 14.51759162 02
| Epoch (UTC): | 13 May 2026 11:44:21 |
| Eccentricity: | 0.0043417 |
| inclination: | 98.6316° |
| perigee height: | 689 km |
| apogee height: | 751 km |
| right ascension of ascending node: | 143.2685° |
| argument of perigee: | 260.5191° |
| revolutions per day: | 14.51759162 |
| mean anomaly at epoch: | 99.1094° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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