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 61241U 26145.59512433 +.00000000 +00000-0 +25978-3 0 00001
2 61241 97.4385 157.0256 0010285 316.8901 43.1532 15.29258407 03
| Epoch (UTC): | 25 May 2026 14:16:58 |
| Eccentricity: | 0.0010285 |
| inclination: | 97.4385° |
| perigee height: | 471 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 157.0256° |
| argument of perigee: | 316.8901° |
| revolutions per day: | 15.29258407 |
| mean anomaly at epoch: | 43.1532° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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