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 31129U 26103.88265308 +.00000000 +00000-0 +15471-3 0 00002
2 31129 98.4501 81.8218 0080621 261.4229 97.7833 14.65758933 04
| Epoch (UTC): | 13 April 2026 21:11:01 |
| Eccentricity: | 0.0080621 |
| inclination: | 98.4501° |
| perigee height: | 618 km |
| apogee height: | 732 km |
| right ascension of ascending node: | 81.8218° |
| argument of perigee: | 261.4229° |
| revolutions per day: | 14.65758933 |
| mean anomaly at epoch: | 97.7833° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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