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 53046U 26145.38316384 +.00000000 +00000-0 +94942-4 0 00007
2 53046 97.4457 326.5212 0001484 84.5560 275.5837 15.05648182 09
| Epoch (UTC): | 25 May 2026 09:11:45 |
| Eccentricity: | 0.0001484 |
| inclination: | 97.4457° |
| perigee height: | 548 km |
| apogee height: | 551 km |
| right ascension of ascending node: | 326.5212° |
| argument of perigee: | 84.5560° |
| revolutions per day: | 15.05648182 |
| mean anomaly at epoch: | 275.5837° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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