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 52694U 26145.35765101 +.00000000 +00000-0 +10718-3 0 00005
2 52694 53.2120 159.9490 0001627 78.5532 281.5643 15.08859817 05
| Epoch (UTC): | 25 May 2026 08:35:01 |
| Eccentricity: | 0.0001627 |
| inclination: | 53.2120° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 159.9490° |
| argument of perigee: | 78.5532° |
| revolutions per day: | 15.08859817 |
| mean anomaly at epoch: | 281.5643° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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