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 26064.91356441 +.00000000 +00000-0 +82887-4 0 00007
2 28538 63.8239 188.2703 0214885 261.0148 96.6505 13.43367834 01
| Epoch (UTC): | 05 March 2026 21:55:31 |
| Eccentricity: | 0.0214885 |
| inclination: | 63.8239° |
| perigee height: | 936 km |
| apogee height: | 1257 km |
| right ascension of ascending node: | 188.2703° |
| argument of perigee: | 261.0148° |
| revolutions per day: | 13.43367834 |
| mean anomaly at epoch: | 96.6505° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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