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 52888U 26145.43669176 +.00000000 +00000-0 +51718-4 0 00000
2 52888 51.9969 131.7147 0000254 328.3336 31.7515 12.62268790 00
| Epoch (UTC): | 25 May 2026 10:28:50 |
| Eccentricity: | 0.0000254 |
| inclination: | 51.9969° |
| perigee height: | 1413 km |
| apogee height: | 1414 km |
| right ascension of ascending node: | 131.7147° |
| argument of perigee: | 328.3336° |
| revolutions per day: | 12.62268790 |
| mean anomaly at epoch: | 31.7515° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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