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 26041.91126535 +.00000000 +00000-0 +81741-4 0 00009
2 28538 63.8220 246.3268 0215094 262.3242 95.3314 13.43365513 01
| Epoch (UTC): | 10 February 2026 21:52:13 |
| Eccentricity: | 0.0215094 |
| inclination: | 63.8220° |
| perigee height: | 936 km |
| apogee height: | 1258 km |
| right ascension of ascending node: | 246.3268° |
| argument of perigee: | 262.3242° |
| revolutions per day: | 13.43365513 |
| mean anomaly at epoch: | 95.3314° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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