▸Orbital parameters

Orbit class	SSO
Inclination	97.6295°
Eccentricity	0.0006399
Period	93.8 min
Apogee	466 km
Perigee	457 km
Mean motion	15.34932512 rev/day
RAAN	329.6399°
Arg of perigee	257.7325°
Mean anomaly	102.3201°
B*	1.7923e-4
Rev at epoch	17,055

▸Two-line element set (TLE)

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

1 56960U 23084AE 26188.14390183 .00005990 00000-0 17923-3 0 9995

2 56960 97.6295 329.6399 0006399 257.7325 102.3201 15.34932512170557

▸ source OMM (JSON)

{
  "OBJECT_NAME": "ORBITER SN3",
  "OBJECT_ID": "2023-084AE",
  "EPOCH": "2026-07-07T03:27:13.118+00:00",
  "MEAN_MOTION": 15.34932512,
  "ECCENTRICITY": 0.0006399,
  "INCLINATION": 97.6295,
  "RA_OF_ASC_NODE": 329.6399,
  "ARG_OF_PERICENTER": 257.7325,
  "MEAN_ANOMALY": 102.3201,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 56960,
  "REV_AT_EPOCH": 17055,
  "BSTAR": 0.00017923,
  "MEAN_MOTION_DOT": 0.0000599,
  "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	ORBITER SN3
Operator	Launcher Inc.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Jun 12, 2023HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	200HIGHvia 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/56960

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