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 61002U 26145.32788708 +.00000000 +00000-0 +17178-4 0 00001
2 61002 53.1602 263.3081 0001016 71.6450 288.4678 15.69720258 00
| Epoch (UTC): | 25 May 2026 07:52:09 |
| Eccentricity: | 0.0001016 |
| inclination: | 53.1602° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 263.3081° |
| argument of perigee: | 71.6450° |
| revolutions per day: | 15.69720258 |
| mean anomaly at epoch: | 288.4678° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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