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 22888U 26103.86249352 +.00000000 +00000-0 +51269-4 0 00009
2 22888 82.9480 128.8229 0048276 8.6764 165.0667 13.75171655 03
| Epoch (UTC): | 13 April 2026 20:41:59 |
| Eccentricity: | 0.0048276 |
| inclination: | 82.9480° |
| perigee height: | 946 km |
| apogee height: | 1017 km |
| right ascension of ascending node: | 128.8229° |
| argument of perigee: | 8.6764° |
| revolutions per day: | 13.75171655 |
| mean anomaly at epoch: | 165.0667° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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