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 52703U 26145.44690513 +.00000000 +00000-0 +44055-4 0 00002
2 52703 53.2136 149.5563 0000825 34.6416 325.4630 15.08849171 08
| Epoch (UTC): | 25 May 2026 10:43:32 |
| Eccentricity: | 0.0000825 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 149.5563° |
| argument of perigee: | 34.6416° |
| revolutions per day: | 15.08849171 |
| mean anomaly at epoch: | 325.4630° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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