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 61201U 26145.32671801 +.00000000 +00000-0 +42362-5 0 00001
2 61201 53.1588 158.6022 0000879 56.4058 303.7044 15.69699091 04
| Epoch (UTC): | 25 May 2026 07:50:28 |
| Eccentricity: | 0.0000879 |
| inclination: | 53.1588° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 158.6022° |
| argument of perigee: | 56.4058° |
| revolutions per day: | 15.69699091 |
| mean anomaly at epoch: | 303.7044° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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