CELTEE 1 is a payload in SSO orbit, operated by US Air Force Research Laboratories/RV (Space Vehicles Directorate), launched 2016.
| Orbit class | SSO |
| Inclination | 98.0649° |
| Eccentricity | 0.0002029 |
| Period | 94.7 min |
| Apogee | 508 km |
| Perigee | 505 km |
| Mean motion | 15.19883845 rev/day |
| RAAN | 55.4525° |
| Arg of perigee | 120.7122° |
| Mean anomaly | 239.4312° |
| B* | 2.2559e-4 |
| Rev at epoch | 52,882 |
1 41850U 16067C 26187.56424572 .00004765 00000-0 22559-3 0 99952 41850 98.0649 55.4525 0002029 120.7122 239.4312 15.19883845528821{
"OBJECT_NAME": "CELTEE 1",
"OBJECT_ID": "2016-067C",
"EPOCH": "2026-07-06T13:32:30.83+00:00",
"MEAN_MOTION": 15.19883845,
"ECCENTRICITY": 0.0002029,
"INCLINATION": 98.0649,
"RA_OF_ASC_NODE": 55.4525,
"ARG_OF_PERICENTER": 120.7122,
"MEAN_ANOMALY": 239.4312,
"EPHEMERIS_TYPE": 0,
"CLASSIFICATION_TYPE": "U",
"NORAD_CAT_ID": 41850,
"REV_AT_EPOCH": 52882,
"BSTAR": 0.00022559,
"MEAN_MOTION_DOT": 0.00004765,
"MEAN_MOTION_DDOT": 0
}Reconstructed from CelesTrak OMM mean-elements (element-set number is a placeholder). TLE/OMM data is approximate. Not for operational use or collision avoidance.
| Name | CELTEE 1 |
| Operator | US Air Force Research Laboratories/RV (Space Vehicles Directorate)HIGHvia GCAT — Jonathan McDowell's General Catalog |
| Country | United States |
| Launch date | |
| Launch mass (kg) | |
| Mission purpose | — |
| Object class | PAYLOADHIGH |
//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.
| Orbital regime |
| Status |