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 52634U 26145.41793124 +.00000000 +00000-0 -93170-5 0 00008
2 52634 53.2128 284.7005 0001140 103.7978 256.3141 15.08845939 04
| Epoch (UTC): | 25 May 2026 10:01:49 |
| Eccentricity: | 0.0001140 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 284.7005° |
| argument of perigee: | 103.7978° |
| revolutions per day: | 15.08845939 |
| mean anomaly at epoch: | 256.3141° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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