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 61202U 26145.44915712 +.00000000 +00000-0 -17963-4 0 00006
2 61202 53.1589 157.9424 0000958 103.6218 256.4907 15.69685434 03
| Epoch (UTC): | 25 May 2026 10:46:47 |
| Eccentricity: | 0.0000958 |
| inclination: | 53.1589° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 157.9424° |
| argument of perigee: | 103.6218° |
| revolutions per day: | 15.69685434 |
| mean anomaly at epoch: | 256.4907° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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