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 28373U 26032.25924108 +.00000000 +00000-0 +19557-3 0 00000
2 28373 98.6956 37.9965 0066169 43.7598 316.8812 14.48914425 02
| Epoch (UTC): | 01 February 2026 06:13:18 |
| Eccentricity: | 0.0066169 |
| inclination: | 98.6956° |
| perigee height: | 682 km |
| apogee height: | 776 km |
| right ascension of ascending node: | 37.9965° |
| argument of perigee: | 43.7598° |
| revolutions per day: | 14.48914425 |
| mean anomaly at epoch: | 316.8812° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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