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 61748U 26145.49755659 +.00000000 +00000-0 +70902-3 0 00008
2 61748 97.2927 23.8044 0004311 28.2546 331.8947 15.64585363 02
| Epoch (UTC): | 25 May 2026 11:56:28 |
| Eccentricity: | 0.0004311 |
| inclination: | 97.2927° |
| perigee height: | 372 km |
| apogee height: | 377 km |
| right ascension of ascending node: | 23.8044° |
| argument of perigee: | 28.2546° |
| revolutions per day: | 15.64585363 |
| mean anomaly at epoch: | 331.8947° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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