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 52334U 26145.41608644 +.00000000 +00000-0 +25643-4 0 00005
2 52334 53.2115 224.6822 0001152 111.4661 248.6454 15.08839275 02
| Epoch (UTC): | 25 May 2026 09:59:09 |
| Eccentricity: | 0.0001152 |
| inclination: | 53.2115° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 224.6822° |
| argument of perigee: | 111.4661° |
| revolutions per day: | 15.08839275 |
| mean anomaly at epoch: | 248.6454° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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