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 53472U 26145.33889140 +.00000000 +00000-0 +10886-3 0 00004
2 53472 97.4469 265.2439 0000901 155.1303 204.9968 15.05647712 07
| Epoch (UTC): | 25 May 2026 08:08:00 |
| Eccentricity: | 0.0000901 |
| inclination: | 97.4469° |
| perigee height: | 549 km |
| apogee height: | 550 km |
| right ascension of ascending node: | 265.2439° |
| argument of perigee: | 155.1303° |
| revolutions per day: | 15.05647712 |
| mean anomaly at epoch: | 204.9968° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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