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 38040U 26088.23699623 +.00000000 +00000-0 +94116-4 0 00007
2 38040 52.0000 260.6802 0000516 96.1402 73.4676 12.62266020 02
| Epoch (UTC): | 29 March 2026 05:41:16 |
| Eccentricity: | 0.0000516 |
| inclination: | 52.0000° |
| perigee height: | 1413 km |
| apogee height: | 1414 km |
| right ascension of ascending node: | 260.6802° |
| argument of perigee: | 96.1402° |
| revolutions per day: | 12.62266020 |
| mean anomaly at epoch: | 73.4676° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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