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 29228U 26098.22323584 +.00000000 +00000-0 +11014-3 0 00000
2 29228 69.9323 160.6222 0002210 25.4723 334.6552 15.12929452 02
| Epoch (UTC): | 08 April 2026 05:21:27 |
| Eccentricity: | 0.0002210 |
| inclination: | 69.9323° |
| perigee height: | 526 km |
| apogee height: | 529 km |
| right ascension of ascending node: | 160.6222° |
| argument of perigee: | 25.4723° |
| revolutions per day: | 15.12929452 |
| mean anomaly at epoch: | 334.6552° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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