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 28811U 26088.05812148 +.00000000 +00000-0 +14597-3 0 00005
2 28811 97.7503 114.1294 0408328 232.4871 123.8528 14.00834233 04
| Epoch (UTC): | 29 March 2026 01:23:41 |
| Eccentricity: | 0.0408328 |
| inclination: | 97.7503° |
| perigee height: | 594 km |
| apogee height: | 1188 km |
| right ascension of ascending node: | 114.1294° |
| argument of perigee: | 232.4871° |
| revolutions per day: | 14.00834233 |
| mean anomaly at epoch: | 123.8528° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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