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 04370U 26064.25078089 +.00000000 +00000-0 +15261-3 0 00002
2 04370 74.0384 129.7539 0015560 311.8461 48.1377 14.63282471 07
| Epoch (UTC): | 05 March 2026 06:01:07 |
| Eccentricity: | 0.0015560 |
| inclination: | 74.0384° |
| perigee height: | 672 km |
| apogee height: | 694 km |
| right ascension of ascending node: | 129.7539° |
| argument of perigee: | 311.8461° |
| revolutions per day: | 14.63282471 |
| mean anomaly at epoch: | 48.1377° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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