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 64552U 26145.58148902 +.00000000 +00000-0 +18226-3 0 00002
2 64552 97.4644 261.0641 0001968 69.3225 290.8222 15.22122672 04
| Epoch (UTC): | 25 May 2026 13:57:20 |
| Eccentricity: | 0.0001968 |
| inclination: | 97.4644° |
| perigee height: | 498 km |
| apogee height: | 501 km |
| right ascension of ascending node: | 261.0641° |
| argument of perigee: | 69.3225° |
| revolutions per day: | 15.22122672 |
| mean anomaly at epoch: | 290.8222° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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