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 23828U 26088.01316596 +.00000000 +00000-0 +56233-4 0 00004
2 23828 99.0515 102.7458 0032815 222.4993 137.3643 14.22667756 04
| Epoch (UTC): | 29 March 2026 00:18:57 |
| Eccentricity: | 0.0032815 |
| inclination: | 99.0515° |
| perigee height: | 793 km |
| apogee height: | 840 km |
| right ascension of ascending node: | 102.7458° |
| argument of perigee: | 222.4993° |
| revolutions per day: | 14.22667756 |
| mean anomaly at epoch: | 137.3643° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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