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 37380U 26039.19463610 +.00000000 +00000-0 +14767-3 0 00002
2 37380 71.9706 73.4454 0015912 347.7320 12.3455 14.84376031 01
| Epoch (UTC): | 08 February 2026 04:40:16 |
| Eccentricity: | 0.0015912 |
| inclination: | 71.9706° |
| perigee height: | 604 km |
| apogee height: | 627 km |
| right ascension of ascending node: | 73.4454° |
| argument of perigee: | 347.7320° |
| revolutions per day: | 14.84376031 |
| mean anomaly at epoch: | 12.3455° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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