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 52849U 26145.41287572 +.00000000 +00000-0 -88831-5 0 00009
2 52849 53.2137 39.6958 0001375 85.5394 274.5755 15.08831730 02
| Epoch (UTC): | 25 May 2026 09:54:32 |
| Eccentricity: | 0.0001375 |
| inclination: | 53.2137° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 39.6958° |
| argument of perigee: | 85.5394° |
| revolutions per day: | 15.08831730 |
| mean anomaly at epoch: | 274.5755° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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