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 55316U 26145.38651910 +.00000000 +00000-0 +54697-4 0 00009
2 55316 69.9985 170.9732 0003923 273.0141 87.0569 14.98320731 05
| Epoch (UTC): | 25 May 2026 09:16:35 |
| Eccentricity: | 0.0003923 |
| inclination: | 69.9985° |
| perigee height: | 569 km |
| apogee height: | 575 km |
| right ascension of ascending node: | 170.9732° |
| argument of perigee: | 273.0141° |
| revolutions per day: | 14.98320731 |
| mean anomaly at epoch: | 87.0569° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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