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 52628U 26145.13870934 +.00000000 +00000-0 -50121-4 0 00003
2 52628 53.2126 300.9270 0001544 95.4757 264.6411 15.08847985 05
| Epoch (UTC): | 25 May 2026 03:19:44 |
| Eccentricity: | 0.0001544 |
| inclination: | 53.2126° |
| perigee height: | 539 km |
| apogee height: | 541 km |
| right ascension of ascending node: | 300.9270° |
| argument of perigee: | 95.4757° |
| revolutions per day: | 15.08847985 |
| mean anomaly at epoch: | 264.6411° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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