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 53248U 26145.47957519 +.00000000 +00000-0 -27545-3 0 00007
2 53248 53.2120 214.5027 0001609 80.8354 279.2820 15.08858533 08
| Epoch (UTC): | 25 May 2026 11:30:35 |
| Eccentricity: | 0.0001609 |
| inclination: | 53.2120° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 214.5027° |
| argument of perigee: | 80.8354° |
| revolutions per day: | 15.08858533 |
| mean anomaly at epoch: | 279.2820° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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