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 36827U 26150.54670818 +.00000000 +00000-0 +12528-3 0 00003
2 36827 98.4344 1.5629 0039922 285.8479 73.8313 14.44809436 09
| Epoch (UTC): | 30 May 2026 13:07:15 |
| Eccentricity: | 0.0039922 |
| inclination: | 98.4344° |
| perigee height: | 714 km |
| apogee height: | 771 km |
| right ascension of ascending node: | 1.5629° |
| argument of perigee: | 285.8479° |
| revolutions per day: | 14.44809436 |
| mean anomaly at epoch: | 73.8313° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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