▸Orbital parameters

Orbit class	SSO
Inclination	97.3841°
Eccentricity	0.0008297
Period	94.5 min
Apogee	499 km
Perigee	487 km
Mean motion	15.24265512 rev/day
RAAN	80.2531°
Arg of perigee	92.7944°
Mean anomaly	267.4243°
B*	2.2596e-4
Rev at epoch	7,290

▸Two-line element set (TLE)

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

1 63235U 25052AB 26188.12025705 .00005450 00000-0 22596-3 0 9991

2 63235 97.3841 80.2531 0008297 92.7944 267.4243 15.24265512 72902

▸ source OMM (JSON)

{
  "OBJECT_NAME": "OTP-2",
  "OBJECT_ID": "2025-052AB",
  "EPOCH": "2026-07-07T02:53:10.209+00:00",
  "MEAN_MOTION": 15.24265512,
  "ECCENTRICITY": 0.0008297,
  "INCLINATION": 97.3841,
  "RA_OF_ASC_NODE": 80.2531,
  "ARG_OF_PERICENTER": 92.7944,
  "MEAN_ANOMALY": 267.4243,
  "EPHEMERIS_TYPE": 0,
  "CLASSIFICATION_TYPE": "U",
  "NORAD_CAT_ID": 63235,
  "REV_AT_EPOCH": 7290,
  "BSTAR": 0.00022596,
  "MEAN_MOTION_DOT": 0.0000545,
  "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	OTP-2
Operator	Rogue Space Systems Corp.HIGHvia GCAT — Jonathan McDowell's General Catalog
Country	United States
Launch date	Mar 15, 2025HIGHvia GCAT — Jonathan McDowell's General Catalog
Launch mass (kg)	11HIGHvia 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/63235

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