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 26144.99913073 +.00000000 +00000-0 +55524-4 0 00008
2 28372 98.6309 155.0931 0043722 224.6179 135.1493 14.51763906 00
| Epoch (UTC): | 24 May 2026 23:58:44 |
| Eccentricity: | 0.0043722 |
| inclination: | 98.6309° |
| perigee height: | 689 km |
| apogee height: | 751 km |
| right ascension of ascending node: | 155.0931° |
| argument of perigee: | 224.6179° |
| revolutions per day: | 14.51763906 |
| mean anomaly at epoch: | 135.1493° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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