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 04362U 26088.02240860 +.00000000 +00000-0 +38838-4 0 00008
2 04362 99.9612 9.8920 0007265 187.7517 183.6498 13.44751017 09
| Epoch (UTC): | 29 March 2026 00:32:16 |
| Eccentricity: | 0.0007265 |
| inclination: | 99.9612° |
| perigee height: | 1086 km |
| apogee height: | 1097 km |
| right ascension of ascending node: | 9.8920° |
| argument of perigee: | 187.7517° |
| revolutions per day: | 13.44751017 |
| mean anomaly at epoch: | 183.6498° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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