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 00202U 26104.04040428 +.00000000 +00000-0 +60492-4 0 00007
2 00202 32.4385 323.6022 0100486 87.6099 273.6022 13.63787271 04
| Epoch (UTC): | 14 April 2026 00:58:10 |
| Eccentricity: | 0.0100486 |
| inclination: | 32.4385° |
| perigee height: | 948 km |
| apogee height: | 1096 km |
| right ascension of ascending node: | 323.6022° |
| argument of perigee: | 87.6099° |
| revolutions per day: | 13.63787271 |
| mean anomaly at epoch: | 273.6022° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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