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 52540U 26145.26153097 +.00000000 +00000-0 +94900-4 0 00006
2 52540 53.2136 145.4158 0001036 70.7628 289.3476 15.08839139 02
| Epoch (UTC): | 25 May 2026 06:16:36 |
| Eccentricity: | 0.0001036 |
| inclination: | 53.2136° |
| perigee height: | 539 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 145.4158° |
| argument of perigee: | 70.7628° |
| revolutions per day: | 15.08839139 |
| mean anomaly at epoch: | 289.3476° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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