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 52487U 26145.49339187 +.00000000 +00000-0 +62605-3 0 00003
2 52487 53.2132 64.4401 0001445 102.7473 257.3681 15.08808881 00
| Epoch (UTC): | 25 May 2026 11:50:29 |
| Eccentricity: | 0.0001445 |
| inclination: | 53.2132° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 64.4401° |
| argument of perigee: | 102.7473° |
| revolutions per day: | 15.08808881 |
| mean anomaly at epoch: | 257.3681° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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