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 52473U 26145.22012194 +.00000000 +00000-0 -15348-3 0 00008
2 52473 53.2128 75.5601 0001603 81.5322 278.5852 15.08854667 06
| Epoch (UTC): | 25 May 2026 05:16:58 |
| Eccentricity: | 0.0001603 |
| inclination: | 53.2128° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 75.5601° |
| argument of perigee: | 81.5322° |
| revolutions per day: | 15.08854667 |
| mean anomaly at epoch: | 278.5852° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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