▸Orbital parameters

Orbit class	SSO
Inclination	97.4515°
Eccentricity	0.0001928
Period	94.7 min
Apogee	507 km
Perigee	504 km
Mean motion	15.20043507 rev/day
RAAN	146.1127°
Arg of perigee	31.9256°
Mean anomaly	328.2095°
B*	4.2325e-4
Rev at epoch	1,493

▸Two-line element set (TLE)

EPOCH Jul 6, 2026SOURCE CelesTrakDERIVED currentUPDATED Jul 7, 2026

1 68429U 26067P 26187.86474622 .00009064 00000-0 42325-3 0 9991

2 68429 97.4515 146.1127 0001928 31.9256 328.2095 15.20043507 14933

▸ source OMM (JSON)

{
  "OBJECT_NAME": "TROOP-F3",
  "OBJECT_ID": "2026-067P",
  "EPOCH": "2026-07-06T20:45:14.073+00:00",
  "MEAN_MOTION": 15.20043507,
  "ECCENTRICITY": 0.0001928,
  "INCLINATION": 97.4515,
  "RA_OF_ASC_NODE": 146.1127,
  "ARG_OF_PERICENTER": 31.9256,
  "MEAN_ANOMALY": 328.2095,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 68429,
  "REV_AT_EPOCH": 1493,
  "BSTAR": 0.00042325,
  "MEAN_MOTION_DOT": 0.00009064,
  "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.

▸Satellite metadata

Name	TROOP-F3
Operator	NearSpaceLaunchHIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Mar 30, 2026HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	10HIGHvia GCAT — Jonathan McDowell's General Catalog
Mission purpose	—
Object class	PAYLOADHIGH

▸Data quality

Score85 / 100

Claims7

Sources1

TLEavailable

▸Sources

GCAT — Jonathan McDowell's General CatalogCC BY 4.0planet4589.org

▸Actions

GET /api/v1/satellites/68429

//Orbital data is approximate and not for operational use. Last ingested from CelesTrak on Jul 7, 2026.