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 37828U 26042.07547086 +.00000000 +00000-0 +57933-3 0 00002
2 37828 49.4550 53.3972 5482492 94.2098 327.0504 4.81548218 04
| Epoch (UTC): | 11 February 2026 01:48:40 |
| Eccentricity: | 0.5482492 |
| inclination: | 49.4550° |
| perigee height: | 314 km |
| apogee height: | 16556 km |
| right ascension of ascending node: | 53.3972° |
| argument of perigee: | 94.2098° |
| revolutions per day: | 4.81548218 |
| mean anomaly at epoch: | 327.0504° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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