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 13844U 26087.76168218 +.00000000 +00000-0 +76450-3 0 00000
2 13844 63.3088 249.4584 0720123 133.5066 232.8191 13.77311139 07
| Epoch (UTC): | 28 March 2026 18:16:49 |
| Eccentricity: | 0.0720123 |
| inclination: | 63.3088° |
| perigee height: | 444 km |
| apogee height: | 1503 km |
| right ascension of ascending node: | 249.4584° |
| argument of perigee: | 133.5066° |
| revolutions per day: | 13.77311139 |
| mean anomaly at epoch: | 232.8191° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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