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 61888U 26145.38465193 +.00000000 +00000-0 +33425-4 0 00002
2 61888 53.1605 129.8665 0001255 91.4307 268.6840 15.34393605 00
| Epoch (UTC): | 25 May 2026 09:13:53 |
| Eccentricity: | 0.0001255 |
| inclination: | 53.1605° |
| perigee height: | 462 km |
| apogee height: | 464 km |
| right ascension of ascending node: | 129.8665° |
| argument of perigee: | 91.4307° |
| revolutions per day: | 15.34393605 |
| mean anomaly at epoch: | 268.6840° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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