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 28538U 26018.53672001 +.00000000 +00000-0 +53872-4 0 00009
2 28538 63.8256 305.3209 0215598 263.6706 93.9731 13.43362906 09
| Epoch (UTC): | 18 January 2026 12:52:52 |
| Eccentricity: | 0.0215598 |
| inclination: | 63.8256° |
| perigee height: | 936 km |
| apogee height: | 1258 km |
| right ascension of ascending node: | 305.3209° |
| argument of perigee: | 263.6706° |
| revolutions per day: | 13.43362906 |
| mean anomaly at epoch: | 93.9731° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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