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 24277U 26080.86441696 +.00000000 +00000-0 +51535-4 0 00008
2 24277 98.8110 134.2069 0001672 47.1865 312.9458 14.30372076 08
| Epoch (UTC): | 21 March 2026 20:44:45 |
| Eccentricity: | 0.0001672 |
| inclination: | 98.8110° |
| perigee height: | 789 km |
| apogee height: | 792 km |
| right ascension of ascending node: | 134.2069° |
| argument of perigee: | 47.1865° |
| revolutions per day: | 14.30372076 |
| mean anomaly at epoch: | 312.9458° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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