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 52362U 26145.42530883 +.00000000 +00000-0 -72364-4 0 00009
2 52362 53.2157 204.6427 0000745 65.6076 294.4994 15.08823019 02
| Epoch (UTC): | 25 May 2026 10:12:26 |
| Eccentricity: | 0.0000745 |
| inclination: | 53.2157° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 204.6427° |
| argument of perigee: | 65.6076° |
| revolutions per day: | 15.08823019 |
| mean anomaly at epoch: | 294.4994° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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