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 28528U 26066.81807177 +.00000000 +00000-0 +15093-2 0 00007
2 28528 49.5134 208.8180 5012647 137.9528 274.0111 5.60265776 00
| Epoch (UTC): | 07 March 2026 19:38:01 |
| Eccentricity: | 0.5012647 |
| inclination: | 49.5134° |
| perigee height: | 300 km |
| apogee height: | 13725 km |
| right ascension of ascending node: | 208.8180° |
| argument of perigee: | 137.9528° |
| revolutions per day: | 5.60265776 |
| mean anomaly at epoch: | 274.0111° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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