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 31490U 26150.13700235 +.00000000 +00000-0 +13935-3 0 00009
2 31490 98.2667 10.1345 0020000 335.7346 24.2923 14.82645571 09
| Epoch (UTC): | 30 May 2026 03:17:17 |
| Eccentricity: | 0.0020000 |
| inclination: | 98.2667° |
| perigee height: | 607 km |
| apogee height: | 635 km |
| right ascension of ascending node: | 10.1345° |
| argument of perigee: | 335.7346° |
| revolutions per day: | 14.82645571 |
| mean anomaly at epoch: | 24.2923° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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