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 03615U 26032.12170545 +.00000000 +00000-0 -67012-4 0 00007
2 03615 101.6840 342.8102 0031656 226.6526 133.1909 12.56247379 09
| Epoch (UTC): | 01 February 2026 02:55:15 |
| Eccentricity: | 0.0031656 |
| inclination: | 101.6840° |
| perigee height: | 1414 km |
| apogee height: | 1463 km |
| right ascension of ascending node: | 342.8102° |
| argument of perigee: | 226.6526° |
| revolutions per day: | 12.56247379 |
| mean anomaly at epoch: | 133.1909° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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